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Aerodynamics
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The concept ** Aerodynamics** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

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

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- 3-D LDV measurements on a 30-degree swept wing with a simulated ice accretion
- A Collection of flow visualization techniques used in the aerodynamic research branch
- A Comparison of the acoustic and aerodynamic measurements of a model rotor tested in two anechoic wind tunnels
- A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel
- A Perspective of computational fluid dynamics
- A comparison of the pitching and plunging response of an oscillating airfoil
- A comparison of the results of dynamic wind-tunnel test with theoretical predictions for an aeromechanical gust-alleviation system for light airplanes
- A comprehensive estimate of the static aerodynamic forces and moments of the 8- by 8- by 20-foot cargo container
- A computational analysis of under-expanded jets in the hypersonic regime
- A computer program to generate equations of motion matrices, L217 (EOM)
- A computionally efficient modelling of laminar separation bubbles
- A consistent spatial differencing scheme for the transonic full-potential equation in three dimensions
- A critical assessment of UH-60 main rotor blade airfoil data
- A critical assessment of wind tunnel results for the NACA 0012 airfoil
- A decade of computer simulations for space shuttle aerodynamics
- A determination of the external forces required to move the benchmark active controls testing model in pure plunge and pure pitch
- A direct-fire trajectory model for supersonic, transonic, and subsonic projectile flight
- A direct-inverse method for transonic and separated flows about airfoils
- A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors : final report
- A first-order time-domain Green's function approach to supersonic unsteady flow
- A general multiblock Euler code for propulsion integration, Volume I, Theory document
- A general multiblock Euler code for propulsion integration, Volume II, User guide for BCON, pre-processor for grid generation and GMBE
- A general multiblock Euler code for propulsion integration, Volume III, User guide for the Euler code
- A geometry package for generation of imput data for a three-dimensional potenial-flow program
- A hybrid numerical technique for predicting the aerodynamic and acoustic fields of advanced turboprops : final report
- A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps
- A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration
- A mathematical formulation of the SCOLE control problem, Part II, Optimal compensator design
- A modern course in aeroelasticity
- A natural low frequency oscillation in the wake of an airfoil near stalling conditions
- A new flux splitting scheme
- A nonlinear investigation of the stationary modes of instability of the three-dimensional compressible boundary layer due to a rotating disc
- A note concerning the onset of three dimensionality and time dependence in Görtler vortices
- A nozzle internal performance prediction method
- A numerical simulation of the NFAC (National Full-Scale Aerodynamics Complex) open-return wind tunnel inlet flow
- A parametric study of accelerations of an airplane due to a wake vortex system
- A practical approach to aircraft flutter analysis
- A program to compute three-dimensional subsonic unsteady aerodynamic characteristics using the doublet lattice method, L216 (DUBFLX)
- A review of 50 years of aerodynamic research with NACA/NASA
- A review of some Reynolds number effects related to bodies at high angles of attack
- A scalable parallel cell-projection volume rendering algorithm for three-dimensional unstructured data
- A slide rule type of device to measure logarithmic decay times as presented by oscillograph records
- A spatial model of wind shear and turbulence for flight simulation
- A streamwise upwind algorithm applied to vortical flow over a deltawing
- A study of artillery shell drift at high angle of fire using solar aspect sensors
- A study of flow past an airfoil with a jet issuing from its lower surface
- A study of high speed flows in an aircraft transition duct
- A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70
- A study of the effects of Reynolds number and mach number on constant pressure coefficient jump for shock-induced trailing-edge separation
- A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results
- A study on vortex flow control on inlet distortion in the re-engined 727-100 center inlet duct using computational fluid dynamics
- A subsonic experimental study of a hypersonic waverider shape
- A supersonic through-flow fan engine airframe integration study
- A three dimensional vortex wake model for missiles at high angles of attack
- A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet
- A unified method of aerospace vehicle dynamic analysis based on tensor concepts
- A user guide for the EMTAC-MZ CFD code
- A viscous flow analysis for the tip vortex generation process
- A water tunnel flow visualization study of the vortex flow structures on the F/A-18 aircraft
- A workshop based simulator for teaching compressible aerodynamics
- A zonal method for modeling powered-lift aircraft flow fields
- ATRAN3S : an unsteady transonic code for clean wings
- Abriss der Lehre von der Flussigkeits- und Gasbewegung
- Accurate multigrid solution of the Euler equations on unstructured and adaptive meshes
- Acoustic and aerodymanics performance of a variable-pitch 1.83-meter- (6-ft.) diameter 1.20-pressure-ratio fan stage (QF-9)
- Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces
- Acquisition and utilization of wind tunnels by the National Aeronautics and Space Administration : report to the Committee on Science and Technology, House of Representatives
- Additional flow field studies of the GA(W)-1 airfoil with 30-percent chord Fowler flap including slot-gap variations and cove shape modifications
- Adjoint methods for aerodynamic wing design : semi-annual progress report
- Admitting the inadmissible : adjoint formulation for incomplete cost functionals in aerodynamic optimization
- Advanced computational fluid and aerodynamics
- Advanced missile technology : a review of technology improvement areas for cruise missiles
- Advanced technology subsonic transport study : N+3 technologies and design concepts
- Advances in dynamics and control
- Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)
- AeroMech : a conceptual design stability and control analysis program
- Aerodonetics, : constituting the second volume of a complete work on aerial flight,
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic analysis of the subsonic ARC-96 trailing wire antenna
- Aerodynamic analysis of wing tip mounted empennages
- Aerodynamic and aerothermodynamic analysis of space mission vehicles
- Aerodynamic characteristcs of a propeller-powered high-lift semispanwing
- Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section
- Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
- Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)
- Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8
- Aerodynamic characteristics of X-15/B-52 combination
- Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement
- Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections
- Aerodynamic characteristics of a propulsive wing/canard concept at STOL speeds
- Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations
- Aerodynamic characteristics of a spoiler-slot-deflector control on a 45° sweptback wing at Mach numbers of 1.61 and 2.01
- Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
- Aerodynamic characteristics of atmospheric boundary layers
- Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience ; prepared for Langley Research Center under contract NAS1-15006
- Aerodynamic characteristics of general aviation at high angle of attack with the propeller slipstream
- Aerodynamic characteristics of several airfoils of low aspect ratio
- Aerodynamic characteristics of sixteen electric, hybrid, and subcompact vehicles : complete data
- Aerodynamic characteristics of the 140A/B space shuttle orbiter at Mach 10.3
- Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)
- Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)
- Aerodynamic characteristics of the National Launch System (NLS) 1 1/2 stage launch vehicle
- Aerodynamic characteristics of the standard dynamics model in coning motion at Mach 0.6
- Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses
- Aerodynamic characteristics of two-dimensional wing configurations at angles of attack near -90?p0 ?s
- Aerodynamic derivatives for both steady and non-steady motion of slender bodies
- Aerodynamic design of transport aircraft
- Aerodynamic design on unstructured grids for turbulent flows
- Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
- Aerodynamic design optimization with sensitivity analysis and computational fluid dynamics
- Aerodynamic design trends for commercial aircraft
- Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model
- Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
- Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers
- Aerodynamic investigation of a cup anemometer
- Aerodynamic loading characteristics in sideslip of a 45° sweptback wing with and without a fence at high subsonic speeds
- Aerodynamic mixing downstream from line source of heat in high-intensity sound field
- Aerodynamic parameter estimation via fourier modulating function techniques
- Aerodynamic parameter studies and sensitivity analysis for rotor blades in axial flight
- Aerodynamic performance of 0.4066-scale model of JT8D refan stage
- Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet
- Aerodynamic performance of flared fan nozzles used as inlets
- Aerodynamic performance of the 17-M-diameter Darrieus wind turbine in the three-bladed configuration : an addendum
- Aerodynamic performance of the 17-metre-diameter Darrieus wind turbine
- Aerodynamic principles of flight vehicles
- Aerodynamic properties of a flat plate with cavity for optical-propagation studies
- Aerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds
- Aerodynamic properties of slender wing-body combinations at subsonic, transonic, and supersonic speeds
- Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
- Aerodynamic theory; : a general review of progress
- Aerodynamic theory; : a general review of progress, under a grant of the Guggenheim fund for the promotion of aeronautics.
- Aerodynamical laboratory.
- Aerodynamics
- Aerodynamics
- Aerodynamics : a space-age survey
- Aerodynamics : constituting the first volume of a complete work on aerial flight..
- Aerodynamics : selected topics in the light of their historical development
- Aerodynamics : selected topics in the light of their historical development
- Aerodynamics for engineering students
- Aerodynamics for engineers
- Aerodynamics for engineers
- Aerodynamics for pilots
- Aerodynamics of Low Reynolds Number Flyers
- Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds
- Aerodynamics of a sphere and an oblate spheroid for Mach numbers from 0.6 to 10.5 including some effects of test conditions
- Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers
- Aerodynamics of engine-airframe interaction : annual progress report
- Aerodynamics of low Reynolds number flyers
- Aerodynamics of low Reynolds number flyers : Wei Shyy ... [et al.]
- Aerodynamics of propulsion/
- Aerodynamics of seeing on large transport aircraft : final technical report, 1 December 1985 through 30 November 1986
- Aerodynamics of slender wings and wing-body combinations having swept trailing edges
- Aerodynamics of the airplane
- Aerodynamics of the airplane,
- Aerodynamics of the helicopter
- Aerodynamics of wings and bodies
- Aerodynamics of wings and bodies
- Aerodynamics,
- Aerodynamics, : a space-age survey
- Aerodynamics, : constituting the first volume of a complete work on aerial flight,
- Aerodynamics, aeronautics, and flight mechanics
- Aerodynamics, the science of air in motion
- Aerodynamics/ACEE
- Aerodynamics: selected topics in the light of their historical development
- Aerodynamik des Fluges;
- Aerodynamik des Flugzeuges
- Aerodynamik und ihre praktische Anwendung am Flugzeug
- Aerodynamik; : ein Gesamtwerk uber das Fliegen,
- Aeroelastic addition to NASTRAN
- Aeroelastic addition to NASTRAN
- Aeroelastic analysis of aircraft : wing and wing/fuselage configurations
- Aeronautical facilities catalogue
- Air Force Academy aeronautics digest
- Air Force Academy aeronautics digest : spring, summer 1981
- Aircraft aerodynamic design : geometry and optimization
- Aircraft aerodynamic design : geometry and optimization
- Aircraft aerodynamic design : geometry and optimization
- Aircraft control by propeller cyclic blades
- Aircraft design
- Aircraft flight dynamics and control
- Aircraft performance : an engineering approach
- Aircraft performance : an engineering approach
- Aircraft performance : theory and practice
- Aircraft performance and sizing
- Aircraft performance and sizing, Volume I, Fundamentals of aircraft performance
- Aircraft performance and sizing, Volume II, Applied aerodynamic design
- Aircraft propulsion, theory and performance; : an introductory text book for students of aeronautics
- Aircraft vibration and flutter,
- Airplane aerodynamics and performance
- Airplane aerodynamics,
- Airplane aerodynamics,
- Airplane design; : aerodynamics,
- Airplane flight dynamics and automatic flight controls
- Airplane performance stability and control.
- Airplane propeller principles,
- American streamlined design : the world of tomorrow
- An Improved panel method for the solution of three-dimensional leading-edge vortex flows
- An aerodynamic model for one and two degree of freedom wing rock of slender delta wings
- An air-flow-direction pickup suitable for telemetering use on pilotless aircraft
- An algebraic homotopy method for generating quasi-three-dimensional grids for high-speed configurations
- An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL)
- An analysis for high Reynolds number inviscid/viscid interactions in cascades
- An analysis of artificial viscosity effects on reacting flows using a spectral multi-domain technique
- An analysis of the crossover between local and massive separation on airfoils
- An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane
- An analysis of the viscous flow through a compact radial turbine by the average passage approach
- An analytical approach to grid sensitivity analysis for NACA four-digit wing sections
- An application of the von Karman-Millikan laminar boundary-layer theory and comparison with experiment
- An efficient algorithm for solution of the unsteady transonic small-disturbance equation
- An entropy correction method for unsteady full potential flows with strong shocks
- An evaluation in a modern wind tunnel of the transonic adaptive wall adjustment developed by NPL in the 1940's
- An experimental analysis of critical factors involved in the breakdown process of leading edge vortex flows
- An experimental and analytical study of the aerodynamic interference effects between two Sears-Haack bodies at Mach 2.7
- An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics
- An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect
- An experimental and theoretical study of the aerodynamic characteristics of some generic missiles concepts at Mach numbers from 2 to 6.8
- An experimental investigation of S-duct flow control using arrays of low profile vortex generators
- An experimental investigation of a supersonic vortical flow
- An experimental investigation of free-tip response to a jet
- An experimental investigation of multi-element airfoil ice accretion and resulting performance degradation
- An experimental investigation of the aerodynamic characteristics of slanted base ogive cylinders using magnetic suspension technology
- An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation
- An experimental investigation of the aerodynamics of a NACA 64A010 airfoil-flap combination with and without flap oscillations : Part 1, Steady-state characteristics
- An experimental investigation of the flap-lag-torsion aeroelastic stability of a small-scale hingeless helicopter rotor in hover
- An experimental investigation of the flow in a diffusing S-duct
- An experimental investigation of thrust vectoring two-dimensional convergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack
- An experimental study of airfoil icing characteristics
- An experimental study of natural and forced modes in an axisymmetric jet
- An experimental study of the aerodynamics of a NACA0012 airfoil with a simulated glaze ice accretion, Volume II
- An experimental study of the aerodynamics of a swept and unswept semispan wing with a simulated glaze ice accretion
- An experimental study of the effect of pitch rate on delta wing aerodynamics and stability : for the period April 1, 1986 - June 30, 1988
- An experimental trace gas investigation of fluid transport and mixing in a circular-to-rectangular transition duct
- An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds
- An exploratory investigation of the STOL landing maneuver
- An improved Woodward's panel method for calculating leading-edge and side-edge suction forces at subsonic and supersonic speed
- An in-flight investigation of ground effect on a forward-swept wing airplane
- An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, January 1, 1988 - June 30, 1988
- An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients : semiannual progress report, July 1991- December 1991
- An interaction algorithm for prediction of mean and fluctuating velocities in two-dimensional aerodynamic wake flows
- An introduction to aerodynamic compressibility
- An introduction to aerodynamic stability
- An introduction to flapping wing aerodynamics
- An introduction to flapping wing aerodynamics
- An introduction to flapping wing aerodynamics
- An introduction to flapping wing aerodynamics
- An introduction to the dynamics of airplanes
- An introduction to the dynamics of airplanes
- An introduction to the theory of aeroelasticity,
- An introduction to theoretical and computational aerodynamics
- An introduction to theoretical and computational aerodynamics
- An investigation of the effects of AFT blowing on a 3.0 caliber tangent Ogive body at high angles of attack
- An investigation of the flow characteristics in the blade endwall corner region
- An unsteady helicopter rotor-fuselage interaction analysis
- Analyses and assessments of span wise gust gradient data from NASA B-57B aircraft
- Analysis of a high speed civil transport configuration at subsonic flow conditions using a Navier-Stokes solver
- Analysis of nonplanar wing-tip-mounted lifting surfaces on low-speed airplanes
- Analysis of selected problems involving vortical flows
- Analysis of supersonic plug nozzle flowfield and heat transfer
- Analysis of vane-type air motors
- Analytical and experimental study of flow phenomena in noncavitating rocket pump inducers
- Analytical determination of flight characteristics of aircraft
- Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades
- Analytical modeling of circuit aerodynamics in the new NASA Lewis Altitude Wind Tunnel
- Analytical modeling of helicopter static and dynamic induced velocity in grasp
- Analytical study of a free-wing/free-trimmer concept
- Ancient China, Masters of the wind and waves
- Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges
- Application of CFD techniques toward the validation of nonlinear aerodynamic models
- Application of Runge Kutta time marching scheme for the computation of transonic flows in turbomachines
- Application of a lower-upper implicit scheme and an interactive grid generation for turbomachinery flow field simulations
- Application of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehicles
- Application of empirical and linear methods to VSTOL powered-lift aerodynamics
- Application of the Bernoulli enthalpy concept to the study of vortex noise and jet impingement noise
- Application of two dimensional unsteady aerodynamics to a free-tip rotor response analysis
- Applications of circulation control technologies
- Applications of circulation control technologies
- Applied aerodynamics : challenges and expectations
- Applied aerodynamics,
- Applied aerodynamics,
- Applied aerodynamics,
- Applied computational aerodynamics
- Applied hydro- and aeromechanics;
- Applied hydro- and aeromechanics; : based on lectures of L. Prandtl.
- Applied hydrodynamics
- Applied wing theory,
- Appraisal of method of flutter analysis based on chosen modes by comparison with experiment for cases of large mass coupling
- Approximation concepts for numerical airfoil optimization
- Atmospheric turbulence, meteorological modeling and aerodynamics
- Automated reduction of data from images and holograms :
- Automatic computation of Euler-marching and subsonic grids forwing-fuselage configurations
- Autonomous momentum management for space station : final report, 15 October 1984
- Average-passage simulation of counter-rotating propfan propulsion systems as applied to Cruise missiles
- BANDSLIP advancements
- Bases theoriques de l'aeronautique.
- Bases theoriques de l'aeronautique. : Aerodynamique; cours professe a l'Ecole imperiale technique de Moscou,
- Basic flight mechanics : a simple approach without equations
- Basic wing and airfoil theory
- Basic wing and airfoil theory
- Bau- und Wirkungsweise des Nimführ-Schwirrfliegers : eine erste Einführung : der Mann und dessen Werk
- Bifurcation theory applied to aircraft motions
- Bifurcation theory applied to aircraft motions
- Bifurcations in unsteady aerodynamics--implications for testing
- Biophysical aerodynamics and the natural environment
- Boundary layer simulator improvement : final report
- Boundary-layer and wake measurements on a swept, circulation-control wing
- Boundary-layer measurements on a transonic low-aspect ratio wing
- Breaking down the delta wing vortex : the role of vorticity in the breakdown
- CFD prediction of Magnus effect in subsonic to supersonic flight
- CFL3D, its history and some recent applications
- Calculation of aerodynamic characteristics of airplane configurations at high angles of attack
- Calculation of aerodynamic characteristics of airplane configurations at high angles of attack : final report
- Calculation of compressible flow about three-dimensional inlets with auxiliary inlets, slats, and vanes by means of a panel method
- Calculation of external-internal flow fields for mixed-compression inlets
- Calculation of non-stationary aerodynamic forces in the near sonic range
- Calculation of steady and unsteady airfoil flow fields via the Navier-Stokes equations
- Calculation of subsonic and supersonic steady and unsteady aerodynamic forces using velocity potential aerodynamic elements
- Calculation of the distributed loads on the blades of individual multiblade propellers in axial flow using linear and nonlinear lifting surface theories
- Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects : User's manual
- Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases
- Calculations of axisymmetric vortex sheet roll-up using a panel and a filament model
- Calculations of hot gas ingestion for a STOVL aircraft model
- Calibration apparatus for recess mounted pressure transducers
- Cascade aerodynamics
- Cascades with harmonically oscillating blades in supersonic flow
- Challenges in simulation of aerodynamics, hydrodynamics, and mooring-line dynamics of floating offshore wind turbines
- Characteristics of loaded fan rotor blade wakes
- Characteristics of supersonic and hypersonic flow over blunt spiked bodies
- Classical aerodynamic theory
- Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine : II - effect of air ejection on turbine performance
- Collected works
- Collected works of Theodore Von Karman, 1952-1963
- Combined aerodynamic and structural dynamic problem emulaing routines (CASPER) : theory and implementation
- Comments regarding two upwind methods for solving two-dimensional external flows using unstructured grids
- Comparison of all-electric secondary power systems for civil subsonic transports
- Comparison of analytical and experimental performance of a wind-tunnel diffuser section
- Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles
- Comparison of numerical flow field predictions for army airdrop systems
- Comparison of theoretical and flight-measured local flow aerodynamics for a low-aspect-ratio fin : final report
- Comparison of two numerical techniques for aerodynamic model identification
- Comparisons of elastic and rigid blade-element rotor models using parallel processing technology for piloted simulations
- Compressibility effects on dynamic stall of airfoils undergoing rapid transient pitching motion
- Computation of three-dimensional effects on two dimensional wings
- Computation of three-dimensional nozzle-exhaust flow fields with the GIM code / L. W. Spradley, P. G. Anderson, and M. L. Pearson
- Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests
- Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests
- Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests : final report
- Computational electromagnetic-aerodynamics
- Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition
- Computational fluid dynamics uses in fluid dynamics/aerodynamics education
- Computational methods in viscous aerodynamics
- Computational model for vortex generators in subsonic internal flows
- Computational results for flows over 2-D ramp and 3-D obstacle with an upwind Navier-Stokes solver
- Computer program to calculate three-dimensional boundary layer over wings with wall mass transfer
- Conceptual design approach for small-caliber aeroballistics with application to 5.56-mm ammunition
- Confined turbulent swirling recirculating flow predictions
- Confined turbulent swirling recirculating flow predictions
- Conical Euler solution for a highly-swept delta wing undergoing wing-rock motion
- Consideration of S. 1267.
- Contributions of numerical simulation data bases to the physics, modeling, and measurement of turbulence
- Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research
- Control of an axisymmetric turbulent jet by multi-modal excitation
- Control of submersible vortex flows
- Control of vortical separation on conical bodies
- Controlling forebody asymmetries in flight : experience with boundary layer transition strips
- Coupled CFD/GN&C modeling for a smart material canard actuator
- Crossflow vorticity sensor : patent application
- Der Flug : ein auf der Wirkung strahlenden Luftdrucks beruhender Vorgang
- Der Luftwiderstand und der flug; : Versuche im Laboratorium des Marsfeldes ausgefuhrt von G. Eiffel, nach der zweiten durchgesehenen und vermehrten Auflage ubersetzt
- Der Schwebflug and die Fallbewegung ebener Tafeln in der Luft : über die Stabilität der Flugapparate
- Der dynamische Flug.
- Design and analysis of advanced flight planning concepts
- Design and calibration of a wind tunnel
- Design and flight evaluation of a new force-based angle probe