#
Computational fluid dynamics
Resource Information
The concept ** Computational fluid dynamics** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

The Resource
Computational fluid dynamics
Resource Information

The concept

**Computational fluid dynamics**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Computational fluid dynamics

- Source
- nasat

## Context

Context of Computational fluid dynamics#### Subject of

- "HPTAM", a two-dimensional heat pipe transient analysis model, including the startup from a frozen state : final report no. UNM-ISNPS-4-1995
- 3-D unstructured method for flows past bodies in 6-DOF relative motion : preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada
- A CFD analysis of hydrogen leakage during on-pad purge in the ORION/ARES I shared volume
- A CFD-based study of the feasibility of adapting an erosion burner rig for examining the effect of CMAS deposition/corrosion on environmental barrier coatings
- A CFD/CSD interaction methodology for aircraft wings : a dissertation ...
- A comparison of interactional aerodynamics methods for a helicopter in low speed flight
- A comparison of lifting-line and CFD methods with flight test data from a research puma helicopter
- A computational fluid dynamics simulation of the hypersonic flight of the Pegasus (TM) vehicle using an artificial viscosity model and a nonlinear filtering method
- A computational investigation of gear windage
- A computational methodology for simulating thermal loss testing of the Advanced Stirling C
- A computational study of multiple jet and wall interaction
- A cost-effective strategy for nonoscillatory convection without clipping
- A dual potential formulation of the Navier-Stokes equations
- A dual potential formulation of the Navier-Stokes equations : final report
- A dual-plane PIV study of turbulent heat transfer flows
- A fast parallel tridiagonal algorithm for a class of CFD applications
- A generalized wall function
- A genuinely multi-dimensional upwind cell-vertex scheme for the Euler equations
- A high order discontinuous Galerkin method for 2D incompressible flows
- A high-order Lagrangian-decoupling method for the incompressible Navier-Stokes equations
- A hybrid numerical method for turbulent mixing layers
- A massively parallel computational approach to coupled thermoelastic/porous gas flow problems
- A method for generating reduced order linear models of supersonic inlets : under grant NAG3-1450
- A method for generating reduced-order linear models of multidimensional supersonic inlets
- A modeling technique for STOVL ejector and volume dynamics
- A non-cut cell immersed boundary method for use in icing simulations
- A novel shape parameterization approach
- A numerical and experimental analysis of reactor performance and deposition rates for CVD on monofilaments
- A numerical method for incompressible flow with heat transfer
- A numerical method for incompressible flow with heat transfer
- A preconditioning method for shape optimization governed by the Euler equations
- A sectored-one-dimensional model for simulating combustion instabilities in premix combustors
- A sectored-one-dimensional model for simulating combustion instabilities in premix combustors
- A semantic analysis method for scientific and engineering code
- A study of pump cavitation damage
- A three-dimensional unsteady CFD model of compressor stability
- A user's guide to CGNS
- Accuracy of schemes with nonuniform meshes for compressible fluid flows
- Accuracy of schemes with nonuniform meshes for compressible fluid flows
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Active control of flow separation over an airfoil
- Adaptive meshing techniques for viscous flow calculations on mixed element unstructured meshes
- Advanced Subsonic Technology (AST) Area of Interest (AOI) 6 : develop and validate aeroleastic [i.e. aeroelastic] codes for turbomachinery
- Advanced low-noise research fan stage design
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ĚŠswept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic design and computational analysis of a spacecraft cabin ventilation fan
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade
- Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level
- Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis : final report for the period ended August 15, 1995
- Aerodynamic synthesis of a centrifugal impeller using CFD and measurements
- Aerodynamic synthesis of a centrifugal impeller using CFD and measurements
- Aeroelastic calculations using CFD for a typical business jet model
- Aeroelastic computations of a compressor stage using the harmonic balance method
- Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications : final report for the period December 1, 1995 through Novemeber 30, 1996
- Aeromechanics analysis of a boundary layer ingesting fan
- An LU implicit scheme for high speed inlet analysis
- An NPARC turbulence module with wall functions : under cooperative agreement NCC3-370
- An adaptive flow solver for air-borne vehicles undergoing time-dependent motions/deformations : annual technical progress report, period--August 1, 1996 - July 31, 1997, NASA grant no.--NAG-1-1760
- An adaptive semi-implicit scheme for simulations of unsteady viscous compressible flows
- An application of the difference potentials method to solving external problems in CFD
- An application of the difference potentials method to solving external problems in CFD
- An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization
- An efficient multiblock method for aerodynamic analysis and design on distributed memory systems : to be presented at the AIAA 13th Computational Fluid Dynamics Conference, June 1997
- An efficient numerical procedure for thermodydrodynamic [sic] analysis of cavitating bearings
- An efficient parallel algorithm for the simulation of three-dimensional compressible transition on a 20 processor Flex/32 multicomputer
- An experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft
- An experimental investigation of a wing-fuselage junction model in the NASA Langley 14- by 22-foot subsonic tunnel
- An implicit, conservative, zonal-boundary scheme for Euler equation calculations
- An incremental strategy for calculating consistent discrete CFD sensitivity derivatives
- An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, July 1, 1987-December 31, 1987
- An inviscid computational study of an X-33 configuration at hypersonic speeds
- Analysis of a hovering rotor in icing conditions
- Analysis of a rocket based combined cycle engine during rocket only operation
- Analysis of buzz in a supersonic inlet
- Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Analysis of lean premixed/prevaporized combustion with KIVA-II
- Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove
- Analysis of the STS-126 flow control valve structural-acoustic coupling failure
- Analytical study of the origin and behavior of asymmetric vortices
- Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995
- Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
- Application of a Runge-Kutta scheme for high-speed inviscid internal flows
- Application of a high-fidelity icing analysis method to a model-scale rotor in forward flight
- Application of an upwind high resolution finite-differencing scheme and multigrid method in steady-state incompressible flow simulations
- Application of low dimensional manifolds in NOx prediction : under cooperative agreement NCC3-534
- Ares I Scale Model Acoustic Test overpressure results
- Artificial boundary conditions based on the difference potentials method
- Artificial boundary conditions based on the difference potentials method
- Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods
- Assessment of NASA's aircraft noise prediction capability
- Assessment of some atomization models used in spray calculations
- Asynchronous communication of TLNS3DMB boundary exchange
- Automated boundary conditions for wind tunnel simulations
- Axial and centrifugal compressor mean line flow analysis method
- Axial-flow turbine rotor discharge-flow overexpansion and limit-loading condition, part 1, Computational fluid dynamics (CFD) investigation
- Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel
- Beta testing of CFD code for the analysis of combustion systems
- Bidirectional brush seals : post-test analysis
- Blended wing body concept development with open rotor engine integration
- Burner rig with an unattached duct for evaluating the erosion resistance of thermal barrier coatings
- CFD analysis and design optimization using parallel computers
- CFD analysis of flexible thermal protection system shear configuration testing in the LCAT facility
- CFD analysis of nozzle jet plume effects on sonic boom signature
- CFD modelling of bore erosion in two-stage light gas guns
- CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report
- CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Capillary channel flow (CCF) EU2-02 on the International Space Station (ISS) : an experimental investigation of passive bubble separations in an open capillary channel
- Cause and cure : deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids
- Combined experimental and numerical simulations of thermal barrier coated turbine blades erosion
- Comments on the diffusive behavior of two upwind schemes
- Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Comparative study of advanced turbulence models for turbomachinery : contract NAS8-38860, final report
- Comparison of NACA 0012 laminar flow solutions : structured and unstructured grid methods
- Comparison of high-order and low-order methods for large-eddy simulation of a compressible shear layer
- Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine
- Comparison of several numerical methods for simulation of compressible shear layers
- Comparison of the booster interface temperature in stainless steel (SS) v-channel versus the aluminum (Al) y-channel Primer Chamber Assemblies (PCAs)
- Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating
- Compliant turbomachine sealing
- Compressible flows with periodic vortical disturbances around lifting airfoils
- Computation of potential flows with embedded vortex rings and applications to helicopter rotor wakes
- Computation of sound generated by viscous flow over a circular cylinder
- Computation of sound generated by viscous flow over a circular cylinder
- Computation of thermally perfect properties of oblique shock waves : under contract NAS1-19000
- Computation of viscous incompressible flows
- Computational Fluid Dynamics (CFD) analysis for the reduction of impeller discharge flow distortion
- Computational Fluid Dynamics (CFD) simulations of jet mixing in tanks of different scales
- Computational aeroacoustics and numerical simulation of supersonic jets : final report on NASA grant NAG 1-1479
- Computational aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development
- Computational aerodynamic simulations of a spacecraft cabin ventilation fan design
- Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development
- Computational analysis of a low-boom supersonic inlet
- Computational analysis of the SSME fuel preburner flow : final report
- Computational analysis of the combustion process in an axisymmetric RBCC flowpath
- Computational analysis of the combustion process in an axisymmetric,RBCC flowpath
- Computational assessment of the aerodynamic performance of a variable-speed power turbine for large civil tilt-rotor application
- Computational fluid dynamics at NASA Ames and the numerical aerodynamic simulation program
- Computational fluid mechanics utilizing the variational principle of modeling damping seals
- Computational icing risk analysis of the D8 "Double Bubble" aircraft
- Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades
- Computational pollutant environment assessment from propulsion-system testing
- Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop
- Computational study of flow establishment in a ram accelerator
- Computational study of near-limit propagation of detonation in hydrogen-air mixtures
- Computational study of near-limit propagation of detonation in hydrogen-air mixtures
- Computational study of separating flow in a planar subsonic diffuser
- Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer
- Computational study of the CC3 impeller and vaneless diffuser experiment
- Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
- Computational work to support FAP/SRW variable-speed power-turbine development
- Computational/experimental aeroheating predictions for X-33 phase II vehicle
- Computations of complex three-dimensional turbulent free jets
- Concept evaluation : NASA reference model 2--side by side
- Connection between the lattice Boltzmann equation and the beam scheme
- Conservational PDF equations of turbulence
- Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers
- Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations
- Convergence analysis of turbulent flow solutions
- Cryogenic fluid storage technology development : recent and planned efforts at NASA
- Current status of superheat spray modeling with NCC
- Data Parallel Line Relaxation (DPLR) code user manual : Acadia version 4.01.1
- Data driven model development for the supersonic semispan transport (S4T)
- Design and analysis of an isokinetic sampling probe for submicron particle measurements at high altitude
- Design and analysis tool for external-compression supersonic inlets
- Detailed experimental data for CFD code validation
- Development and demonstration of a computational tool for the analysis of particle vitiation effects in hypersonic propulsion test facilities
- Development and life prediction of erosion resistant turbine low conductivity thermal barrier coatings
- Development and validation of a multidisciplinary tool for accurate and efficient rotorcraft noise prediction (MUTE)
- Development of a fluid structures interaction test technique for fabrics
- Development of an axisymmetric afterbody test case for turbulent flow separation validation
- Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations : final technical report
- Development of an upwind, finite-volume code with finite-rate chemistry
- Development of detonation modeling capabilities for rocket test facilities : hydrogen-oxygen-nitrogen mixtures
- Development of improved surface integral methods for jet aeroacoustic predictions : final report, NASA-Langley grant no. NAG-1660
- Development of the Glenn Heat-Transfer (Glenn-HT) computer code to enable Time-Filtered Navier-Stokes (TFNS) simulations and application to film cooling on a flat plate through long cooling tubes
- Development of three-dimensional DRAGON grid technology
- Development of three-dimensional DRAGON grid technology
- Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D
- Direct numerical simulation of a temporally evolving incompressible plane wake : effect of initial conditions on evolution and topology
- Direct numerical simulation of incompressible pipe flow using a B-spline spectral method
- Direct numerical simulation of incompressible pipe flow using a b-spline spectral method
- Directional agglomeration multigrid techniques for high-Reynolds number viscous flows
- Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization : final report for the period ended September 30, 1995
- Drag reduction on circular cylinders by ejecting jet from rear stagnation region : progress report for the period ending June 30, 1997 ... under Cooperative Agreement NCC1-232
- Dual-pump CARS development and application to supersonic combustion
- Duct flow nonuniformities study for Space Shuttle main engine : technical report
- Dynamic stall suppression using combustion-powered actuation (COMPACT)
- Dynamics of large-scale structures for jets in crossflow
- Dynamics of superfluid helium in low-gravity : NASW-4803, final report
- Effect of coannular flow on linearized Euler equation predictions of jet noise
- Effect of curvature on the impact damage characteritiscs and residual strength of composite plates : presented at 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference : Long Beach, California, April 20-23, 1998
- Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan
- Efficient gradient-based shape optimization methodology using inviscid/viscous CFD : summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211
- Efficient grid generation : final report
- Efficient implementation of weighted ENO schemes
- Efficient parallel kernel solvers for computational fluid dynamics applications : final report, NASA contract no. NAG1-1672 (Jan. 1995-Aug. 97)
- Energy transfer and triadic interactions in compressible turbulence : under contract NAS1-19480
- Enhanced multiobjective optimization technique for comprehensive aerospace design : final report on NCC2-5150
- Enhancing aeropropulsion research with high-speed interactive computing
- Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing
- Essential elements of computational algorithms for aerodynamic analysis and design : under contracts NAS1-97046 & NAS1-19480
- Euler flow computations on non-matching unstructured meshes
- Euler technology assessment : SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts
- Euler technology assessment for preliminary aircraft design : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration
- Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
- Evaluation of CFD turbulent heating prediction techniques and comparison with hypersonic experimental data
- Evaluation of inflow turbulence methods in large-eddy simulations of a supersonic boundary layer
- Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics : prepared for 2018 SciTech Forum spnsored by the American Institute of Aeronautics and Astronautics Kissimmee, Florida, January 8-12, 2018
- Exhaust nozzle plume and shock wave interaction
- Exhaust nozzle plume effects on sonic boom test results for isolated nozzles
- Exhaust nozzle plume effects on sonic boom test results for vectored nozzles
- Experimental and computational aerothermodynamics of a Mars entry vehicle
- Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle
- Experimental and computational sonic boom assessment of Boeing N+2 low boom models
- Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models
- Experimental database with baseline CFD solutions : 2-D and axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions
- Experimental investigation of Mars Science Laboratory entry vehicle aeroheating in AEDC hypervelocity tunnel 9
- Explicit and implicit compact high-resolution shock-capturing methods for multidimensional Euler equations I, formulation
- Extension of a kinetic approach to chemical reactions to electronic energy levels and reactions involving charged species with application to DSMC simulations
- Extension of an object-oriented optimization tool : use's reference manual
- Extension of transonic flow computational concepts in the analysis of cavitated bearings
- External boundary conditions for three-dimensional problems of computational aerodynamics
- External boundary conditions for three-dimensional problems of computational aerodynamics
- F-16XL-2 supersonic laminar flow control flight test experiment
- FUN3D manual, 12.5
- Fan noise source diagnostic test computation of rotor wake turbulence noise
- Fan noise source diagnostic test computation of rotor wake turbulence noise
- Film temperatures in the presence of cavitation
- Final report for parallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997
- Final report for the shuttle flight experiment on USMP-4 : in situ monitoring of crystal growth using MEPHISTO
- Flat plate wake velocity statistics obtained with circular and elliptic trailing edges
- Flight test results on the stability and control of the F-15 Quiet Spike aircraft
- Flight testing the linear aerospike SR-71 experiment (LASRE)
- Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
- Flow analysis of the Cleveland clinic centrifugal pump
- Flow analysis of the Cleveland clinic centrifugal pump
- Flow control under low-pressure turbine conditions using pulsed jets : final report
- Fluid acquisition and resupply experiments on space shuttle flights STS-53 and STS-57
- Forced mixer nozzle optimization
- Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
- Fuel injector design optimization for an annular scramjet geometry
- Full-scale direct numerical simulation of two- and three-dimensional instabilities and rivulet formation in heated falling films : /
- Fundamental ice crystal accretion physics studies
- Fundamental study of a single point lean direct injector part I : effect of air swirler angle and injector tip location on spray characteristics
- Funding and strategic alignment guidance for infusing small business innovation research technology into NASA programs associated with the Human Exploration and Operations Mission Directorate
- Further development of a method for computing three-dimensional subsonic viscous flows in turbofan lobe mixers
- Further validation of a CFD code for calculating the performance of two-stage light gas guns
- Generation of performance model for the Aeolian Wind Tunnel (AWT) rotor at reduced pressure
- Geometry and simulation results for a gas turbine representative of the energy efficient engine (EEE)
- Global artificial boundary conditions for computation of external flow problems with propulsive jets
- Globalized Newton-Krylov-Schwarz algorithms and software for parallel implicit CFD
- Heat transfer computations of internal flows with combined hydraulic and thermal developing length
- Heat transfer on a film-cooled rotating blade
- Helicopter blade-vortex interaction noise with comparisons to CFD calculations
- Helicopter blade-vortex interaction noise with comparisons to CFD calculations
- Helicopter rotor blade computation in unsteady flows using moving overset grids
- High fidelity CFD analysis and validation of rotorcraft gearbox aerodynamics under operational and oil-out conditions : final report
- High order finite difference and finite volume WENO schemes and discontinuous Galerkin methods for CFD
- High-order space-time methods for conservation laws
- Higher-order compact schemes for numerical simulation of incompressible flows
- Hydrodynamic design of the fastrac turbopump
- Hypersonic pitching-moment shift for stardust reentry capsule forebody
- Ice crystal icing research at NASA
- Ice-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel
- Impact of an exhaust throat on semi-idealized rotating detonation engine performance
- Impact of load balancing on unstructured adaptive grid computations for distributed-memory multiprocessors
- Implementation of a multiblock sensitivity analysis method in numerical aerodynamic shape optimization : abstract
- Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade
- Implicit schemes and parallel computing in unstructured grid CFD
- Improvements to an explicit algebraic stress model for turbulent jet mixing predictions
- Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ĚŠangle of attack : contract NAS 3-26617
- Inspection of the Math Model Tools for on-orbit assessment of impact damage report
- Interaction of sound from supersonic jets with nearby structures
- Interactive algebraic grid-generation technique
- Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Inverse design technique for cascades
- Investigation of active flow control to improve aerodynamic performance of oscillating wings
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
- Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
- Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
- Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
- Isolated rotor forward flight testing at Martian atmospheric density data report
- Jet noise reduction potential from emerging variable cycle technologies
- Krylov methods for compressible flows
- LES of a jet excited by the Localized Arc Filament Plasma Actuators
- LSPRAY : a Lagrangian spray solver, user's manual : prepared under contract NAS3-27186
- LSPRAY-IV : a lagrangian spray module
- Large-scale parallel viscous flow computations using an unstructured multigrid algorithm
- Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller
- Linear instability of a uni-directional transversely sheared mean flow
- Long hole film cooling dataset for CFD development, Part 1, Infrared thermography and thermocouple surveys
- Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects
- Magnetically actuated propellant orientation experiment, controlling fluid motion with magnetic fields in a low-gravity environment : (MSFC Center Director's Discretionary Fund final report, project no. 93-18)
- Mars entry atmospheric data system modeling, calibration, and error analysis
- Mars sample return : Mars Ascent Vehicle mission & technology requirements
- Mass transfer from a sphere in an oscillating flow with zero mean velocity
- Mathematical analysis of the Navier-Stokes equations with non standard boundary conditions
- Mean velocity and turbulence measurements in a 90Â° curved duct with thin inlet boundary layer : final report
- Mean veoIocity and turbulence measurements in a 900 curved duct with thin inlet boundary layer : final report
- Measuring global surface pressures on a circulation control concept using pressure sensitive paint
- Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995
- Methodology for simulation of unsteady flows to determine the time-dependent interference between stationary and moving boundaries : [abstract
- Methods for computationally efficient structured CFD simulations of complex turbomachinery flows
- Micro-ramp flow control for oblique shock interactions : comparisons of computational and experimental data
- Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept
- Mir cooperative solar array flight performance data and computational analysis
- Mixing enhancement by tabs in round supersonic jets
- Modeling of turbulent swirling flows
- Modeling vortex generators in the Wind-US Code
- Multi-partitioning for ADI-schemes on message passing architectures
- Multidisciplinary design optimization using multiobjective formulation techniques : final report on NASA Ames grant no. NCA2-778
- Multigrid method for stability problems
- Multigrid method for stability problems : final report
- Multigrid methods for aerodynamic problems in complex geometries : final report
- Multiphysics simulation of active hypersonic lip cooling
- Multiple scales approach to weakly nonparallel and curvature effects : details for the novice
- Multiple-cycle simulation of a pulse detonation engine ejector
- NASA Rotor 37 CFD code validation : Glenn-HT code
- NASA numerical and experimental evaluation of UTRC low emissions injector
- NASA one-dimensional combustor simulation : user manual for S1D_ML
- National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program - 1995 : grant NGT 44-001-800
- National combustion code parallel performance enhancements
- Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing
- Navier-Stokes computations on full wing-body configuration with oscillating control surfaces
- Navier-Stokes simulation of several high-lift reference H configurations
- Nearly interactive Parabolized Navier-Stokes solver for high speed forebody and inlet flows
- New computational methods for the prediction and analysis of helicopter noise
- Nonlinear (time domain) and linearized (title & freqency domain) solutions to the compressible Euler equations in conservation law form : final report for NASA Lewis Research Center
- Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model
- Nonlinear dynamics & numerical uncertainties in CFD
- Nozzle flow with vibrational nonequilibrium : final report for the period ended August 31, 1995
- Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel
- Numerical analysis of a rotating detonation engine in the relative reference frame
- Numerical assessment of four-port through-flow wave rotor cycles with passage height variation
- Numerical flow visualization in basic- and hyper-cluster spheres
- Numerical simulation methods of incompressible flows and an application to the space shuttle main engine
- Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
- Numerical simulation of low-density shock-wave interactions
- Numerical simulation of low-density shock-wave interactions
- Numerical simulation of scramjet inlet flow fields
- Numerical simulation of vitiation effects on a hydrogen-fueled dual-mode scramjet
- Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design
- Numerical simulations of two-phase reacting flow in a single-element lean direct injection (LDI) combustor using NCC
- Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
- Numerical study of boundary-layer control in aerodynamics : final technical report for grant NCC 2-845, NASA-Ames Research Center; grant period: 1 January 1994 to 31 December 1995, no-cost extension to 31 December 1996
- Numerical study of stratified charge combustion in wave rotors
- Numerically simulating an expanding continuum jet into a surrounding non-continuum region
- Observations on computational methodologies for use in large-scale, gradient-based, multidisciplinary design incorporating advanced CFD codes
- Observations regarding use of advanced CFD analysis, sensitivity analysis, and design codes in MDO
- On approximate factorization schemes for solving the full potential equation
- On convergence acceleration techniques for unstructured meshes
- On formulations of discontinuous Galerkin and related methods for conservation laws
- On multifunctional collaborative methods in engineering science
- On the application of chimera/unstructured hybrid grids for conjugate heat transfer
- Optical characterization of a multipoint lean direct injector for gas turbine combustors : velocity and fuel drop size measurements
- Optimization of an advanced design three-element airfoil at high Reynolds numbers
- Orion Service Module Reaction Control System plume impingement analysis using PLIMP/RAMP2
- Oscillating flow and heat transfer in a channel with sudden cross section change : final report
- Overview of ICE project : integration of computational fluid dynamics and experiments
- Overview of heat addition and efficiency predictions for an advanced stirling convertor
- Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project
- Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project
- PARC3D calculations of the F/A-18A HARV inlet vortex generators
- PIV and rotational Raman-based temperature measures for CFD validation in a single injector cooling flow
- PLOT3D user's manual
- PLTTER user's guide
- PLTTER user's guide
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Parallel Newton-Krylov-Schwarz algorithms for the transonic full potential equation : NASA contract no. NAS1-19480
- Parallel aeroelastic computations for wing and wing-body configurations : annual report for the period of time July 1993-July 1994
- Parallel implementation of an adaptive scheme for 3D unstructured grids on the SP2
- Parallelization of the implicit RPLUS algorithm : final report, NASA grant NAG 3-1472
- Parallelized modelling and solution scheme for hierarchically scaled simulations : final report
- Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
- Parametric study of decay of homogeneous isotropic turbulence using large eddy simulation
- Particle kinetic simulation of high altitude hypervelocity flight : periodic research report for the period February 1, 1992 - December 31, 1992
- Passive rocket diffuser testing : reacting flow performance of four second-throat geometries
- Passive rocket diffuser theory : a re-examination of minimum second throat size
- Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
- Performance evaluation of the NASA GTX RBCC flowpath
- Performance gains of propellant management devices for liquid hydrogen depots
- Performance impact of deflagration to detonation transition enhancing obstacles
- Performance of the widely-used CFD code OVERFLOW on the Pleides supercomputer
- Physics of forced unsteady separation : proceedings of a NASA/AFOSR/ARO workshop held at NASA Ames Research Center, Moffett Field, California, April 17-19, 1990
- Planar Inlet Design and Analysis Process (PINDAP)
- Potential application of NASA aerospace technology to ground-based power systems
- Potential application of NASA aerospace technology to ground-based power systems
- Potential theoretic methods for far field sound radiation calculations
- Preconditioning methods for low-speed flows
- Predicting turbulent convective heat transfer in three-dimensional duct flows
- Prediction of complex aerodynamic flows with explicit algebraic stress models : 34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV
- Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn
- Preliminary aerodynamic investigation of fan rotor blade morphing
- Preprocessor that enables the use of GridPro grids for unsteady Reynolds-averaged Navier-Stokes code TURBO
- Production level CFD code acceleration for hybrid many-core architectures
- Progress in grid generation : from chimera to DRAGON grids
- Progress of high efficiency centrifugal compressor simulations using TURBO
- Prospects for CFD on petaflops systems
- Pseudo-time method for optimal shape design using the Euler equations
- Quiet, efficient fans for spaceflight : an overview of NASA's technology development plan
- Radiation-spray coupling for realistic flow configurations
- Rapid prediction of unsteady three-dimensional viscous flows in turbopump geometries : progress report 2
- Recalibration of the shear stress transport model to improve calculation of shock separated flows
- Recent development in the CESE method for the solution of the Navier-Stokes Equations using unstructured triangular or tetrahedral meshes with high aspect ratio
- Reduced Navier Stokes relaxation procedures for internal flows : final report, NASA grant no. NAG3-397, 3/01/83-2/28/96
- Reentry-F flowfield solutions at 80,000 ft.
- Requirements for large eddy simulation computations of variable-speed power turbine flows
- Research applied to transonic compressors in numerical fluid mechanics of inviscid flow and viscous flow : final technical report for Grant no. NAG 3-9 submitted to the NASA Lewis Research Center, Cleveland, OH 44135
- Research in computational aeroscience applications implemented on advanced parallel computing systems : final report for first year of prime contract NAS2-14090
- Research in parallel algorithms and software for computational aerosciences : report NAS TR 96-004
- Research in progress : applied and numerical mathematics : semiannual report, October 1, 1995 through March 31, 1996
- Research on supersonic inlet bleed
- Results and current status of the NPARC alliance validation effort
- Results of an advanced fan stage operating over a wide range of speed and bypass ratio : comparison of CFD and experimental results, part 2
- Review of Godunov methods
- Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments
- Rocket-based combined cycle engine technology development : inlet CFD validation and application
- Role of computational fluid dynamics and wind tunnels in aeronautics R&D
- RotCFD analysis of the AH-56 Cheyenne hub drag
- Rotor CFD analysis at terrestrial and martian atmospheric densities
- Rotor vortex filaments : living on the slipstream's edge
- Rotor vortex filaments : living on the slipstream's edge
- SRM internal flow test and computational fluid dynamic analyses : final report, contract NAS8-39095
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- Secondary frequencies in the wake of a circular cylinder with vortex shedding
- Semi-span model testing in the National Transonic Facility : annual status report, August 1995, cooperative agreement no. NCC1, 169
- Seventh Copper Mountain Conference on Multigrid Methods
- Shape optimization of single- and two-element airfoils on multiblock grids
- Shock wave interaction with an abrupt area change
- Simulation of VSPT experimental cascade under high and low free-stream turbulence conditions
- Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral
- Simulations of spray reacting flows in a single element LDI injector with and without invoking an Eulerian scalar PDF method
- Simulations of the Mars helicopter test propeller in hover configuration at Martian pressure and air density
- Slot nozzle effects for reduced sonic boom on a generic supersonic wing section
- SmaggIce : surface modeling and grid generation for iced airfoils, phase I results
- Small engine technology (set) Task 8, aeroelastic prediction methods : final report : prepared under contract NAS3-27483
- Small scale mass flow plug calibration
- Solar thermal upper stage liquid hydrogen pressure control testing
- Solar thermal upper stage liquid hydrogen pressure control testing and analytical modeling
- Some developments of the equilibrium particle simulation method for the direct simulation of compressible flows
- Space Shuttle Program (SSP) orbiter main propulsion system (MPS) gaseous hydrogen (GH2) flow control valve (FCV) poppet eddy current (EC) inspection probability of detection (POD) study
- Spreadsheet calculation of jets in crossflow : opposed rows of slots slanted at 45Â°
- Stability of a rigid rotor supported on oil-film journal bearings under dynamic load
- Status, emerging ideas and future directions of turbulence modeling research in aeronautics
- Steady-state and transient boundary element methods for coupled heat conduction
- Steady-state and transient boundary element methods for coupled heat conduction
- Stirling analysis comparison of commercial versus high-order methods
- Study of basic physical processes in liquid rocket engines
- Study of basic physical processes in liquid rocket engines
- Study of the TRAC airfoil table computational system
- Study of the mutual interaction between a wing wake and an encountering airplane : NASA grant no. NAG1-1572, final report
- Study of two-dimensional compressible non-acoustic modeling of stirling machine type components
- Summary of EASM turbulence models in CFL3D with validation test cases
- Summary of EASM turbulence models in CFL3D with validation test cases
- Summary report of the orbital X-34 wing static aeroelastic study
- Supersonic wind tunnel tests of a half-axisymmetric 120-spike inlet to a rocket-based combined-cycle propulsion system
- Supersonic wind tunnel tests of a half-axisymmetric 12Â°-spike inlet to a rocket-based combined-cycle propulsion system
- Supersonic wing and wing-body shape optimization using an adjoint formulation
- Swept wing ice accretion modeling
- TADS--a CFD-based turbomachinery analysis and design system with GUI : version 2.0--methods and results
- TADS--a CFD-based turbomachinery analysis and design system with GUI : version 2.0--user's manual
- Ten years in the making : AUSM-family
- Textbook multigrid efficiency for the incompressible Navier-Stokes equations : high Reynolds number wakes and boundary layers
- The NASA subsonic jet particle image velocimetry (PIV) dataset
- The aerospace plane design challenge : credible computational fluid dynamics results
- The development of a tool for semi-automated generation of structured and unstructured grids about isolated rotorcraft blades
- The effect of wake passing on turbine blade film cooling
- The implicit and explicit a-u [i.e. alpha-mu] schemes
- The interactions of a flame and its self-induced boundary layer
- The research and training activities for the joint Institute for Aeronautics and Acoustics : submitted to the NASA Ames Research Center for a period of one year, October 1, 1997 to September 30, 1998
- The role of computational fluid dynamics at Marshall Space Flight Center : presented at Emerging Horizons of Turbomachinery Technology, Wilder, Vermont, May 11-15, 1998
- The second ICASE/LaRC Industry Roundtable : session proceedings
- The sound of moving bodies
- The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws, II, Numerical simulation of shock waves and contact discontinuities
- The stability of two-dimensional wakes and shear-layers at high Mach numbers
- The variational method for aerodynamic optimization using the Navier-Stokes equations : prepared for Langley Research Center under contract NAS1-19480
- Theoretical aeroacoustics : compiled mathematical derivations of Fereidoun 'Feri' Farassat
- Three-dimensional aerodynamic shape optimization of supersonic delta wings : [abstract]
- Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis : abstract
- Three-dimensional high-lift analysis using a parallel unstructured multigrid solver
- Three-dimensional simulation of vortex breakdown
- Time-filtered Navier-Stokes approach and emulation of turbulence-chemistry interaction
- Totally parallel multilevel algorithms
- Toward automatic verification of goal-oriented flow simulations
- Training knowledge bots for physics-based simulations using artificial neurals networks
- Transonic investigation of two-dimensional nozzles designed for supersonic cruise
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, GĂ¶ttingen, Germany, September 16-18, 1996
- Turbulence modeling : progress and future outlook
- Turbulence modeling validation, testing, and development
- Turbulent fluid motion V : fourier analysis, the spectral form of the continuum equations, and homogeneous turbulence
- Turbulent fluid motion VI : turbulence, nonlinear dynamics, and deterministic chaos
- Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade
- Two-step multi-physics analysis of an annular linear induction pump for fission power systems
- Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses
- Unsteady aero computation of a 1 1/2 stage large scale rotating turbine
- Unstructured adaptive grid computations on an array of SMPs
- Unstructured grid Euler method assessment for longitudinal and lateral/directional aerodynamic performance analysis of the HSR technology concept airplane at supersonic cruise speeds
- Unstructured grid Euler method assessment for longitudinal and lateral/directional stability analysis of the HSR Reference H configuration at transonic speeds
- Updates to simulation of a single-element lean-direct injection combustor using a polyhedral mesh derived from hanging-node elements
- User's manual for FOMOCO utilities : Force and Moment Computation tools for overset grids
- Using computers in fluids engineering education
- Using numerical simulations to explore top-mounted propulsion on a conceptual commercial supersonic transport aircraft
- Validation of WIND for a series of inlet flows
- Validation of WIND for a series of inlet flows
- Validation of a CFD methodology for variable speed power turbine relevant conditions
- Validation tests of TASS for application to 3-D vortex simulations
- Verification and improvement of flamelet approach for non-premixed flames : summary report under cooperative agreement no. NCC3-496, with NASA Lewis Research Center; period of implementation--September 1996-August 1997
- Vibration dissociation coupling in nonequilibrium flows : final report on consortium agreement NCA2-519
- Virtual and experimental visualization of flows in packed beds of spheres simulating porous media flows
- Virtual and experimental visualization of flows in packed beds of spheres simulating porous media flows
- Viscous compressible flow direct and inverse computation with illustrations
- Visual Computing Environment Workshop
- Visualization and tracking of parallel CFD simulations : report NAS-95-004
- Visualization of flows in packed beds of twisted tapes
- Visualization of unsteady Computational Fluid Dynamics : final technical report for grant #NAG2-884
- Visualization of unsteady computational fluid dynamics : final technical report for grant #NAG2-884
- Visualizing turbulent mixing of gases and particles
- Vortex perturbation dynamics
- WRLES : wave resolving large-eddy simulation code, theory and usage
- Wave augmented diffusers for centrifugal compressors
- Wave augmented diffusers for centrifugal compressors
- Wind code application to external forebody flowfields with comparisons to experimental results
- Wind tunnel interference effects on tiltrotor testing using computational fluid dynamics
- Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop
- Wind-US user's guide
- Wing-section optimization for supersonic viscous flow : [abstract]
- X-34 experimental aeroheating at Mach 6 and 10
- [Analysis and development of finite element methods for the study of nonlinear thermomechanical behavior of structural components]

## Embed (Experimental)

### Settings

Select options that apply then copy and paste the RDF/HTML data fragment to include in your application

Embed this data in a secure (HTTPS) page:

Layout options:

Include data citation:

<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.libraries.ou.edu/resource/Mwb83Ju25ow/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.libraries.ou.edu/resource/Mwb83Ju25ow/">Computational fluid dynamics</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.libraries.ou.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.libraries.ou.edu/">University of Oklahoma Libraries</a></span></span></span></span></div>

Note: Adjust the width and height settings defined in the RDF/HTML code fragment to best match your requirements

### Preview

## Cite Data - Experimental

### Data Citation of the Concept Computational fluid dynamics

Copy and paste the following RDF/HTML data fragment to cite this resource

`<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.libraries.ou.edu/resource/Mwb83Ju25ow/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.libraries.ou.edu/resource/Mwb83Ju25ow/">Computational fluid dynamics</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.libraries.ou.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.libraries.ou.edu/">University of Oklahoma Libraries</a></span></span></span></span></div>`