Aerofoils
Resource Information
The concept Aerofoils represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
The Resource
Aerofoils
Resource Information
The concept Aerofoils represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
- Label
- Aerofoils
- Authority link
- (EG-IN)1251839
177 Items that share the Concept Aerofoils
Context
Context of AerofoilsSubject of
No resources found
No enriched resources found
- [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
Embed
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.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>
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 Aerofoils
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.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>
