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Aerofoils
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The concept ** Aerofoils** represents the subject, aboutness, idea or notion of resources found in **Indiana State Library**.

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Aerofoils
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The concept

**Aerofoils**represents the subject, aboutness, idea or notion of resources found in**Indiana State Library**.- Label
- Aerofoils

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- (EG-IN)1251839

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- [The Structure of separated flow regions occurring near the leading edge of airfoils, including transition]
- A comparison of Wortmann airfoil computer-generated lift and drag polars with flight and wind tunnel results
- 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 computer program for estimating the areodynamic characteristics of NACA 16-series airfoils
- A computionally efficient modelling of laminar separation bubbles
- A flow visualization study of the leading edge separation bubble on a NACA 0012 airfoil with simulated glaze ice
- A lifting surface theory in rotational flow
- A low speed two-dimensional study of flow separation on the GA(W)-1 airfoil with 30-percent chord fowler flap
- 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 rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
- A recontoured, upper surface designed to increase the maximum lift coefficient of a modified NACA 65 (0.82) (9.9) airfoil section
- 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 turbulence model for iced airfoils and its validation
- 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
- Additional flow field studies of the GA(W)-1 airfoil with 30-percent chord Fowler flap including slot-gap variations and cove shape modifications
- Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section
- Aerodynamic characteristics of a rotorcraft airfoil designed for the tip region of a main rotor blade
- Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses
- Aileron effectiveness for a subsonic transport model with a high-aspect-ratio supercritical wing
- Airfoil design by numerical optimization using a minicomputer
- Airfoil interaction with an impinging vortex
- An Experimental investigation of a supercritical airfoil at transonic speeds
- An airfoil pitch apparatus : modeling and control design
- An analysis of the crossover between local and massive separation on 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 mapping of the flow field behind a glaze ice shape on a NACA 0012 airfoil
- An exploratory investigation of the effect of a plastic coating on the profile drag of a practical-metal-construction sailplane airfoil
- 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 strong-interaction dynamic stall for laminar flow on airfoils
- Analysis of transitional separation bubbles on infinite swept wings
- Analysis of unswept and swept wing chordwise pressure data from an oscillating NACA 0012 airfoil experiment
- Application of a nonisentropic full potential method to AGARD standard airfoils
- Application of shock tubes to transonic airfoil testing at high Reynolds number
- Approximation concepts for numerical airfoil optimization
- 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
- 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
- Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application
- 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
- Computations of two-dimensional airfoil-vortex interactions
- Control of "laminar separation" over airfoils by acoustic excitation
- Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel
- Correlation of laser velocimeter measurements over a wing with results of two prediction techniques
- Data from tests of a R4 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift
- 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
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section
- 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
- Estimation of unsteady lift on a pitching airfoil from wake velocity surveys
- Experimental and theoretical low-speed aerodynamic characterisitics of a Wortmann airfoil as manufactured on a fiberglass sailplane
- Experimental ice shape and performance characteristics for a multi-element airfoil in the NASA Lewis Icing Research Tunnel
- Experimental investigation of the flowfield of an oscillating airfoil
- 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 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 the separating confluent boundary-layer
- Experimental verification of a new laminar airfoil : a project for the graduate program in aeronautics : final report
- 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
- 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 evaluation of the transonic stability and control characteristics of an airplane incorporating a supercritical wing
- Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap
- Further wind tunnel investigation of the SM701 airfoil with aileron and turbulators
- Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis Icing Research Tunnel
- 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
- Icing characteristics of a natural-laminar-flow, a medium-speed, and a swept,medium-speed airfoil
- Icing test results on an advanced two-dimensional high-lift multi-element airfoil
- Improved methods of vibration analysis of pretwisted, airfoil blades
- Interacting boundary-layer solutions for laminar separated flow past airfoils
- Interaction of a surface wave with a dielectric slab discontinuity
- Inverse transonic airfoil design methods including boundary layer and viscous interaction effects : semiannual progress report, September 1, 1983 -- January 31, 1984
- Investigation of blown boundary layers with an improved wall jet system
- 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
- 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
- Leading-edge slat optimization for maximum airfoil lift
- Life prediction and constitutive models for engine hot section anisotropic materials program : annual status report
- 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 wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
- 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 631-012 airfoil
- Measurement of local convective heat transfer coefficients from a smooth and roughened NACA-0012 airfoil : flight test data
- 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
- Numerical approach for the aerodynamic analysis of airfoils with laminar separation
- 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 studies of porous airfoils in transonic flow : final report
- On the flow processes in sharply inclined and stalled airfoils in parallel movement and rotation
- On the validation of a code and a turbulence model appropriate to circulation control airfoils
- Operational manual for two-dimensional transonic code TSFOIL
- 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
- Prediction of ice shapes and their effect on airfoil performance
- 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
- Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model
- Separated transonic airfoil flow calculations with a nonequilibrium turbulence model
- Simulation of transonic separated airfoil flow by finite-difference viscous-inviscid interaction
- 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
- Study of controlled diffusion stator blading : final report, II
- Study of transonic flow over swept wings : final technical report
- 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
- 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 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 : design overview
- The construction of airfoil pressure models by the bonded plate method : achievements, current research, technology development and potential applications
- The low frequency oscillation in the flow over a NACA0012 airfoil with an "iced" leading edge
- The status of analytical preparation for 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, November 1984 - April 1985
- Three-dimensional effects on airfoils
- Transient technique for measuring heat transfer coefficients on stator airfoils in a jet engine environment
- Transonic calculation of airfoil stability and response with active controls
- 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 wind tunnel test of an oscillating rotor airfoil, volume I
- 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"
- Verification of performance results for a low-speed 15% eliptical circulation control airfoil
- Viscous effects on transonic airfoil stability and response
- 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 results for a high-speed, natural laminar-flow airfoil designed for general aviation aircraft
- Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
- [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]
- 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

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`<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/kHeIm6xYMyw/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/kHeIm6xYMyw/">Aerofoils</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>`