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

The Resource
Aerofoils
Resource Information

The concept

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

## Context

Context of Aerofoils#### Subject of

- 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
- A New method of evaluating the side wall interference effect on airfoil angle of attack by suction from the side walls
- A Search for 183-GHz emission from water in late-type stars
- A Two element laminar flow airfoil optimized for cruise
- A comparison of Wortmann airfoil computer-generated lift and drag polars with flight and wind tunnel results
- A comparison of computer-generated lift and drag polars for a Wortman airfoil to flight and wind tunnel results : final report
- A comparison of design variables for control theory based airfoil optimization
- A comparison of two central difference schemes for solving the Navier-Stokes equations
- A compendium of controlled diffusion blades generated by an automated inverse design procedure
- A computionally efficient modelling of laminar separation bubbles
- A computionally efficient modelling of laminar separation bubbles : semi-annual status report, June 1988 - January 1989 for NASA grant NAG-1-778
- A direct-inverse method for transonic and separated flows about airfoils
- A far-field non-reflecting boundary condition for two-dimensional wake flows
- A flow visualization study of the leading edge separation bubble on a NACA 0012 airfoil with simulated glaze ice
- A fundamental study of the sticking of insect residues to aircraft wings : annual technical report
- A general representation for axial-flow fans and turbines
- A laser-based ice shape profilometer for use in icing wind tunnels
- A low speed two-dimensional study of flow separation on the GA(W)-1 airfoil with 30-percent chord fowler flap
- A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution
- A natural low frequency oscillation in the wake of an airfoil near stalling conditions
- A numerical study of the effects of wind tunnel wall proximity on an airfoil model
- A preconditioning method for shape optimization governed by the Euler equations
- A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
- A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
- A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel
- A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form
- A study of flow past an airfoil with a jet issuing from its lower surface
- A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel
- A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow
- A thin wing in a compressible flow
- A turbulence model for iced airfoils and its validation
- A two dimensional study of rotor/airfoil interaction in hover
- A verification of unsteady Navier-Stokes solutions around oscillating airfoils
- Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence
- Acoustic radiation from lifting airfoils in compressible subsonic flow
- Acoustic scattering from ellipses by the modal element method
- Active control of flow separation over an airfoil
- Additional flow field studies of the GA(W)-1 airfoil with 30-percent chord Fowler flap including slot-gap variations and cove shape modifications
- Advanced ice protection systems test in the NASA Lewis Icing Research Tunnel
- 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 NACA 0012 airfoil section at angles of attack from 0 to 180 degrees
- Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections
- Aerodynamic characteristics of a rotorcraft airfoil designed for the tip region of a main rotor blade
- Aerodynamic characteristics of several airfoils of low aspect ratio
- 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 two NASA supercritical airfoils with different maximum thicknesses
- Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7
- Aerodynamic data banks for Clark-Y, NACA 4-digit, and NACA 16-series airfoil families
- Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil
- Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section
- Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
- Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds
- Aerothermal modeling : phase 1 - final report : executive summary
- Aileron effectiveness for a subsonic transport model with a high-aspect-ratio supercritical wing
- Airfoil design and data
- Airfoil design by numerical optimization using a minicomputer
- Airfoil in sinusoidal motion in a pulsating stream
- Airfoil interaction with an impinging vortex
- Airfoil lift with changing angle of attack
- Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range
- Airfoil section characteristics at high angles of attack
- An Experimental investigation of a supercritical airfoil at transonic speeds
- An Integrating manometer for use in wind tunnel pressure distribution measurements
- An airfoil pitch apparatus : modeling and control design
- An analysis of base pressure at supersonic velocities and comparison with experiment
- An analysis of estimated and experimental transonic downwash characteristics as affected by plan form and thickness for wing and wing-fuselage configurations
- An analysis of the crossover between local and massive separation on airfoils
- An approach to the constrained design of natural laminar flow airfoils
- An experimental investigation of gapwise periodicity and unsteady aerodynamic response in an oscillating cascade
- An experimental investigation of multi-element airfoil ice accretion and resulting performance degradation
- 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 confluent boundary layer on a high-lift system : final project report
- An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer
- An experimental investigation of two 15%-scale wind tunnel fan-blade designs
- An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil, and a NACA 64-210 airfoil in simulated heavy rain : final report to the NASA Langley Research Center on work accomplished under research grant NAG-1-568
- An experimental mapping of the flow field behind a glaze ice shape on a NACA 0012 airfoil
- An experimental study of the aerodynamics of a NACA 0012 airfoil with a simulated glaze ice accretion
- An experimental study of the aerodynamics of a NACA0012 airfoil with a simulated glaze ice accretion, Volume II
- An exploratory investigation of the effect of a plastic coating on the profile drag of a practical-metal-construction sailplane airfoil
- An improved viscid/inviscid interaction procedure for transonic flow over airfoils
- An integrated optimum design approach for high speed prop rotors : final report on NASA Ames grant no. NCC2-795
- An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0
- An investigation of the flow characteristics in the blade endwall corner region
- Analysis of airfoil transitional separation bubbles
- Analysis of low-speed unsteady airfoil flows
- Analysis of strong-interaction dynamic stall for laminar flow on airfoils
- Analysis of two-dimensional incompressible flow past airfoils using unsteady Navier-Stokes equations
- Analysis of unswept and swept wing chordwise pressure data from an oscillating NACA 0012 airfoil experiment
- Annual progress report ... entitled "an experimental investigation of the flow physics of high-lift systems" for the period March-December 1995
- Application of a nonisentropic full potential method to AGARD standard airfoils
- Application of shock tubes to transonic airfoil testing at high Reynolds number
- Applications of circulation control technologies
- Applications of circulation control technologies
- Applied wing theory,
- Approximation concepts for numerical airfoil optimization
- Artificial boundary conditions for computation of oscillating external flows
- Assessment of two-equation turbulence models for transonic flows
- Attainable circulation of airfoils in cascade
- Basic wing and airfoil theory
- Basic wing and airfoil theory
- Blade loss transient dynamics analysis with flexible bladed disk
- Boundary-fitted curvilinear coordinate systems for solution of partial differential equations on fields containing any number of arbitrary two-dimensional bodies
- Calculation of boundary layers of oscillating airfoils
- Calculation of steady and unsteady airfoil flow fields via the Navier-Stokes equations
- Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness
- Calibration of averaging total pressure flight wake rake and natural-laminar-flow airfoil drag certification
- Characteristics of a separating confluent boundary layer and the downstream wake
- Characteristics of merging shear layers and turbulent wakes of a multi-element airfoil
- Charts for estimation of the characteristics of a helicopter rotor in forward flight : 1 - Profile drag-lift ratio for untwisted rectangular blades
- Charts of pressure rise obtainable with airfoil-type axial-flow cooling fans
- Closed-loop separation control using oscillatory flow excitation
- Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Comparison of computational and experimental results for a supercritical airfoil
- Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application
- Comparison of several dissipation algorithms for central difference schemes
- Comparison of the full-potential and Euler formulations for computing transonic airfoil flows
- Computation of full-coverage film-cooled airfoil temperatures by two methods and comparison with high heat flux data
- Computational aeroeleastic investigation of a membrane airfoil undergoing figure of eight motion
- Computations of two-dimensional airfoil-vortex interactions
- Computer program to obtain ordinates for NACA airfoils
- Continued development and application of circulation control pneumatic technology to advanced transport aircraft : NASA grant NAG-1-1517 : period covered, June 14, 1993 to August 31, 1997
- Control of "laminar separation" over airfoils by acoustic excitation
- Control of separated flow past a cylinder using tangential wall jet blowing
- Control of unsteady separated flow associated with the dynamic stall of airfoils
- Control of unsteady separated flow associated with the dynamic stall of airfoils : final report, 95-09
- Control theory based airfoil design for potential flow and a finite volume discretization
- Control theory based airfoil design using the Euler equations
- Correlation of laser velocimeter measurements over a wing with results of two prediction techniques
- Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds
- Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack : final report
- Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
- DRA/NASA/ONERA collaboration on icing research, Part II, Prediction of airfoil ice accretion
- Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations
- Data from tests of a R4 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment
- Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow
- Development and testing of airfoils for high-altitude aircraft : final report
- Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift
- Die aeroplane und luftschrauben der statischen und dynamischen luftschiffahrt schwerer und leichter als luft. : Eine gemeinverstandliche beschreibung ihrer anordnung und anleitung zu ihrer berechnung fur konstrukteure, luftschiffer und liebhaber,
- Die beste Tragdeck-form und der Luftwiderstand; : eine leichtfassliche Entwicklung der Luftwirkungs-gesetze für Flugtechniker und Freunde physikalischer Naturbetrachtung,
- Distributed-roughness effects on stability and transition in swept-wing boundary layers : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing Company contract #ZA0078, during 5/17/96-12/31/96
- Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization : final report for the period ended September 30, 1995
- Dynamic stall experiments on the NACA 0012 airfoil
- Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model
- Effect of an extendable slat on the stall behavior of a VR-12 airfoil
- Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing
- Effect of aspect ratio on undamped torsional oscillations of a thin rectangular wing in supersonic flow
- Effect of in-flight ice accretion on the performance of a multi-element airfoil
- Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
- Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections
- Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60
- Effects of compressibility on maximum lift coefficients for six propeller airfoils
- Effects of environmentally imposed roughness on airfoil performance
- Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section
- Effects of suction on swept-wing transition : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998
- Effects of upper surface modification on the aerodynamic characteristics of the NACA 632-215 airfoil section
- Energy efficient engine high-pressure turbine detailed design report
- Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the Mach lines
- Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves
- Estimation of the damping in roll of rings through the normal flight range of lift coefficient
- Estimation of unsteady lift on a pitching airfoil from wake velocity surveys
- Evaluation of constant-Weber-number scaling for icing tests
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow
- Experimental analyses of trailing edge flows : final technical report to NASA Ames Research Center
- Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
- Experimental and theoretical low-speed aerodynamic characteristics of a Wortmann airfoil as manufactured on a fiberglass sailplane
- Experimental determination of aerodynamic characteristics of a model airplane with annular airfoils
- Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model
- Experimental ice shape and performance characteristics for a multi-element airfoil in the NASA Lewis Icing Research Tunnel
- Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
- Experimental investigation of the flowfield of an oscillating airfoil
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet
- Experimental investigations on airfoils with different geometries in the domain of high angles of attack - flow separation
- Experimental measurements of the laminar separation bubble on an Eppler 387 airfoil at low Reynolds numbers : final report
- Experimental optimization methods for multi-element airfoils : final report
- Experimental results for a flapped natural-laminar-flow airfoil with high lift/drag ratio
- Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel
- Experimental studies of flow separation of three airfoils at low speeds
- Experimental study of complex vortex interactions in the wake of high aspect ratio wings : final report on NASA grant NAG-1-1816
- Experimental study of the separating confluent boundary-layer
- Experimental verification of a new laminar airfoil : a project for the graduate program in aeronautics : final report
- Extension of the theory of oscillating airfoils of finite span in subsonic compressible flow
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Feasability of predicting performance degradation of airfoils in heavy rain
- Feedback in separated flows over symmetric airfoils
- Final report for modeling of heavy-gas effects on airfoil flows
- Final report for the period January 1, 1974 through December 31, 1983 entitled : Numerical solution of the Navier-Stokes equations for arbitrary two-dimensional multi-element airfoils
- Final report on study of organized structures in the post-stall flow over wings
- Flight Mechanics/Estimation Theory Symposium, 1989 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989
- Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Flight evaluation of the transonic stability and control characteristics of an airplane incorporating a supercritical wing
- Flow simulations about steady-complex and unsteady moving configurations using structured-overlapped and unstructured grids : abstract
- Flutter at very high speeds
- Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap
- Formulas and tables of coefficients for numerical differentiation with function values given at unequally spaced points and application to solution of partial differential equations
- Fowler flaps for airplanes, : an engineering handbook
- Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
- Further evaluation of traditional icing scaling methods
- Further investigations of icing effects on an advanced high-lift multi-element airfoil
- Further wind tunnel investigation of the SM701 airfoil with aileron and turbulators
- GRUMFOIL, a computer code for the viscous transonic flow over airfoils
- Global artificial boundary conditions for computation of external flow problems with propulsive jets
- Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis Icing Research Tunnel
- Helicopter tail rotor noise analyses
- High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II
- High Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- High lift, low pitching moment airfoils : patent application
- Historical background and design evolution of the transonic aircraft technology supercritical wing
- ICEG2D (v2.0) : an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- Ice accretion with varying surface tension
- Ice accretions and icing effects for modern airfoils
- Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark Y airfoil
- Icing characteristics of a natural-laminar-flow, a medium-speed, and a swept,medium-speed airfoil
- Icing simulation : a survey of computer models and experimental facilities
- Icing test results on an advanced two-dimensional high-lift multi-element airfoil
- Implementation of a multiblock sensitivity analysis method in numerical aerodynamic shape optimization : abstract
- Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
- Improved methods of vibration analysis of pretwisted, airfoil blades
- Impulsive start of a symmetric airfoil at high angle of attack
- Interacting boundary-layer solutions for laminar separated flow past airfoils
- Interaction of a surface wave with a dielectric slab discontinuity
- Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps
- Investigation of a simple device for preventing separation due to shock and boundary-layer interaction
- Investigation of blown boundary layers with an improved wall jet system
- Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65-series wings equipped with full-span slotted flaps
- Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction : final report
- Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction : semi-annual report for the period March 16, 1983 to September 14, 1983
- Inviscid analysis of two supercritical laminar-flow-control airfoils at design and off-design conditions
- Isolated and cascade airfoils with prescribed velocity distribution
- Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions
- Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions
- KC-135 Winglet Program Review : proceedings of a symposium held at Dryden Flight Research Center, Edwards, California, September 16, 1981
- Kasprzyk airfoil : the first wind-tunnel tests
- Key topics for high-lift research : a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996
- Leading-edge slat optimization for maximum airfoil lift
- Life prediction and constitutive models for engine hot section anisotropic materials program : final report
- Life prediction and constitutive models for engine hot section anisotropic materials program : second annual status report
- Low-speed aerodynamic characteristics of a 16-percent thick variable-geometry airfoil designed for general aviation applications
- Low-speed experimental investigation of a thin, faired, double-wedge airfoil section with nose and trailing-edge flaps
- Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
- MATE program : erosion resistant compressor airfoil coating, Volume II
- Materials for Advanced Turbine Engines (MATE) : project 4--erosion resistant compressor airfoil coating
- Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63-012 airfoil
- Measurement of local convective heat transfer coefficients from a smooth and roughened NACA-0012 airfoil : flight test data
- Measurements in the boundary layer of a yawed wing
- Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data
- Method of characteristic studies for rotational flow downstream of a curved shock wave
- Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995
- Modern airfoil ice accretions
- NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
- NASA supercritical airfoils : a matrix of family-related airfoils
- Natural laminar flow airfoil design considerations for winglets on low-speed airplanes
- Navier-Stokes analysis of airfoils with leading edge ice accretions
- Note on the accuracy of a method for rapidly calculating the increments in velocity about an airfoil due to angle of attack
- Numerical computation of viscous flow about unconventional airfoil shapes : final report
- Numerical modeling of anti-icing systems and comparison to test results on a NACA 0012 airfoil
- Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
- Numerical simulation of the SOFIA flowfield
- Numerical solutions of the complete Navier-Stokes equations : progress report no. 27 for the period October 1, 1995 to September 30, 1996
- Numerical studies of porous airfoils in transonic flow : final report
- Numerical study of turbulence model predictions for the MD 30P/30N and NHLP-2D three-element highlift configurations
- On the Second-order tunnel-wall-constriction corrections in two-dimensional compressible flow
- On the validation of a code and a turbulence model appropriate to circulation control airfoils
- Operational manual for two-dimensional transonic code TSFOIL
- Optimization with variable-fidelity models applied to wing design
- Optimum aerodynamic design via boundary control
- Optimum transonic airfoils based on the Euler equations
- Oscillating airfoils and their wake
- Porous plug for reducing orifice induced pressure error in airfoils : patent application
- Potential flow analysis of glaze ice accretions on an airfoil : [final report]
- Potential flow around two-dimensional airfoils using a singular integral method
- Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
- Prediction of film cooling on gas turbine airfoils
- Prediction of ice shapes and their effect on airfoil performance
- Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight : final technical report under NASA-Ames research grant no. NAG 2-797
- Preliminary indications of water film distribution and thickness on an airfoil in a water spray
- Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Rapport d'essais du profil CAST 10 en transition dʹeclenchʹee, effectuʹes dans la soufflerie transsonique cryogʹenique T2 en pr'esence de parois auto-adaptables : Report on tests of a CAST 10 airfoil with fiexed transition in the T2 transonic cryogenic wind tunnel with self-adaptive walls
- Report on the special field "interference" to the wind tunnel committee in February 1945
- Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model
- Robust airfoil optimization to achieve consistent drag reduction over a mach range
- Separated transonic airfoil flow calculations with a nonequilibrium turbulence model
- Shape optimization of single- and two-element airfoils on multiblock grids
- SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions
- Similarity laws for transonic flow about wings of finite span
- Simulation of a controlled airfoil with jets
- Simulation of transonic separated airfoil flow by finite-difference viscous-inviscid interaction
- SmaggIce user guide : SmaggIce version 1.0
- SmaggIce, surface modeling and grid generation for iced airfoils : phase 1 results
- Spanwise spacing effects on the initial structure and decay of axial vortices : under contract NAS3-27377
- Spatial and temporal adaptive procedures for the unsteady aerodynamic analysis of airfoils using unstructured meshes
- Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility
- Structural analysis of injection molded composite fan blades
- Structural tailoring of engine blades (STAEBL), theoretical manual
- Structural tailoring of engine blades (STAEBL), user's manual
- Study of controlled diffusion stator blading : final report, II
- Study of the TRAC airfoil table computational system
- Study of transonic flow over swept wings : final technical report
- Stuttgarter Profilkatalog
- Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall
- Supercritical flow past a symmetrical bicircular arc airfoil
- Suppression of dynamic stall with a leading-edge slat on a VR-7 airfoil
- Swept wing attachment line contamination fence
- TADS, a CFD-based turbomachinery and analysis design system with GUI
- TADS--a CFD-based turbomachinery analysis and design system with GUI : version 2.0--methods and results
- TRANSEP, a program for high lift separated flow about airfoils
- Tables for correcting airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel for sidewall boundary layer effects
- Technology for pressure-instrumented thin airfoil models
- Tests in the Variable Density Wind Tunnel to investigate the effects of scale and turbulence on airfoil characteristics
- Tests on a CAST 7 two-dimensional airfoil in a self-streamlining test section
- The Effects of leading edge and downstream film cooling on turbine vane heat transfer
- The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil : basic results for slotted configuration
- The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview
- The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction
- The aerodynamic characteristics of six commonly used airfoils over a large range of positive and negative angles of attack
- The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
- The decay of longitudinal vortices shed from airfoil vortex generators
- The effect of a change in airfoil section on the hinge-moment characteristics of a half-delta tip control with a 60° sweep angle at a Mach number of 6.9
- The effects of sideslip, aspect ratio, and Mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow
- The effects of the critical ice accretion on airfoil and wing performance : NASA contract # NCC3-408 : January 24, 1995-November 30, 1996 : final report
- The elements of aerofoil and airscrew theory
- The elements of aerofoil and airscrew theory
- The elements of aerofoil and airscrew theory
- The elements of aerofoil and airscrew theory
- The flying machine; : two papers: The aerofoil and The Screw propeller.
- The influence of free-stream turbulence on separation of turbulent boundary layers in incompressible, two-dimensional flow : final report
- The low frequency oscillation in the flow over a NACA0012 airfoil with an "iced" leading edge
- The method of complex characteristics for design of transonic blade sections
- The paths of soaring flight
- The reversibility theorem for thin airfoils in subsonic and supersonic flow
- The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil : final technical report
- The status of analytical preparation for two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel
- The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel
- The structure of separated flow regions occuring near the leading edge of airfoils including transition
- The structure of separated flow regions occurring near the leading edge of airfoils, including transition : semi-annual status report, February 1986-July 1986
- The structure of separated flow regions occurring near the leading edge of airfoils, including transition : semi-annual status report, November 1984 - April 1985
- The yawing moment, due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow
- Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow
- Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds
- Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow
- Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
- Theory of wing sections : including a summary of airfoil data
- Thermal barrier coating life-prediction model development : second annual report
- Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis : abstract
- Trandesnf : a computer program for transonic airfoil design and analysis in nonuniform flow
- Transient aerodynamic behavior of an airfoil due to different arbitrary modes of nonstationary motions in a supersonic flow
- Transient technique for measuring heat transfer coefficients on stator airfoils in a jet engine environment
- Transonic interference reduction by limited ventilation wall panels
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996
- Transonic wind-tunnel investigation of the maneuver potential of the NASA supercritical wing concept : phase I
- Turbine blade and vane heat flux sensor development phase 1
- Two experimental supercritical laminar-flow-control swept-wing airfoils
- Two-dimensional aerodynamic characteristics of an airfoil designed for rotorcraft application
- Two-dimensional aerodynamic characteristics of the Ames HI-120, HI-8, and LOW-12 airfoils
- Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil
- Two-dimensional aerodynamic characteristics of three rotorcraft airfoils at mach numbers from 0.35 to 0.90
- Two-dimensional cold-air cascade study of a film-cooled turbine stator blade
- Two-dimensional high-lift aerodynamic optimization using neural networks
- Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
- Two-dimensional transonic flow past airfoils
- Two-dimensional wind tunnel test of an oscillating rotor airfoil, volume I
- Unsteady cascade aerodynamic response using a multiphysics simulation code
- Unsteady pressure measurements on a biconvex airfoil in a transonic oscillating cascade
- Unsteady transonic aerodynamic and aeroelastic calculations about airfoils and wings
- Use of a liquid-crystal, heater-element composite for quantitative, high-resolution heat transfer coefficients on a turbine airfoil, including turbulence and surface roughness effects
- User's manual for airfoil flow field computer code "SRAIR"
- User's manual for the NASA Lewis ice accretion/heat transfer prediction code with electrothermal deicer input
- Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility
- Velocity distributions on arbitrary airfoils in closed tunnels by conformal mapping
- Velocity distributions on symmetrical airfoils in closed tunnels by conformal mapping
- Verification of performance results for a low-speed 15% elliptical circulation control airfoil
- Viper
- Volterra's solution of the wave equation as applied to three-dimensional supersonic airfoil problems
- Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section
- Water-tunnel experiments on an oscillating airfoil at RE = 21,000
- Wind tunnel aerodynamic characteristics of a transport-type airfoil in a simulated heavy rain environment
- Wind tunnel evaluation of a truncated NACA 64-621 airfoil for wind turbine applications
- Wind tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing : 1- Aileron with fixed inset tabs
- Wind tunnel investigation of control surface characteristics : 12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance
- Wind tunnel investigations of the new 7380 semi-rigid airfoil
- Wind tunnel results for a high-speed, natural laminar-flow airfoil designed for general aviation aircraft
- Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons
- Wind-tunnel investigation of ailerons on a low-drag airfoil : 1 - The effect of aileron profile
- Wind-tunnel investigation of ailerons on a low-drag airfoil : 2 - The effect of thickened and beveled trailing edges
- Wind-tunnel investigation of shielded horn balancees and tabs on a 0.7-scale model of XF6F vertical tail surface
- Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps
- Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
- Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modification of aileron nose and adjacent airfoil contour
- Wing theory
- Wing theory,
- Wing-section optimization for supersonic viscous flow : [abstract]
- Wing-section optimization for supersonic viscous flows : abstract
- [Life prediction and constitutive models for engine hot section anisotropic materials program] : [interim report]
- [Solution of separated flows using a simultaneous iteration technique] : [final report]
- [The Structure of separated flow regions occurring near the leading edge of airfoils, including transition]
- Über den Luftwiderstand gekrummeter flächen

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