Airfoils

286 books
Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoilJames C. Ferris
⏱ 35m

Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil

James C. Ferris

198735 pp.
The influence of free-stream turbulence on separation of turbulent boundary layers in incompressible, two-dimensional flowUnknown Author

The influence of free-stream turbulence on separation of turbulent boundary layers in incompressible, two-dimensional flow

Unknown Author

1986No page data
Airfoil self-noise and predictionThomas F. Brooks
⏱ 2h 17m

Airfoil self-noise and prediction

Thomas F. Brooks

1989137 pp.
Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoilMichael E. Watts
⏱ 1h 28m

Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil

Michael E. Watts

198888 pp.
Evaluation of constant-Weber-number scaling for icing testsDavid N. Anderson

Evaluation of constant-Weber-number scaling for icing tests

David N. Anderson

1996No page data
Multi-element airfoil optimization for maximum lift at high Reynolds numbersWalter O. Valarezo
⏱ 16h 16m

Multi-element airfoil optimization for maximum lift at high Reynolds numbers

Walter O. Valarezo

1991976 pp.
Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil liftGaudy M. Bezos
⏱ 1h 5m

Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift

Gaudy M. Bezos

199365 pp.
A transonic-small-disturbance wing design methodologyPamela S. Phillips
⏱ 28m

A transonic-small-disturbance wing design methodology

Pamela S. Phillips

198828 pp.
Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnelCharles D. Harris
⏱ 2h 17m

Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel

Charles D. Harris

1981137 pp.
NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnelRenaldo V. Jenkins
⏱ 55m

NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel

Renaldo V. Jenkins

198955 pp.
Interactive airfoil calculations with higher-order viscous flow equationsD. W. Zingg
⏱ 8h 46m

Interactive airfoil calculations with higher-order viscous flow equations

D. W. Zingg

1990526 pp.
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic TunnelWilliam G. Johnson
⏱ 4h 26m

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

William G. Johnson

1985266 pp.
Airfoil computation at high angles of attack, inviscid and viscous phenomenaJohn T. Barton
⏱ 21m

Airfoil computation at high angles of attack, inviscid and viscous phenomena

John T. Barton

198421 pp.
Nonlinear unsteady airfoil response studiesG. W. Johnston
⏱ 12m

Nonlinear unsteady airfoil response studies

G. W. Johnston

198912 pp.
Inverse methods for airfoil design for aeronatuical and turbomachinery applicationsNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 4h 15m

Inverse methods for airfoil design for aeronatuical and turbomachinery applications

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1990255 pp.
CAST-10-2/DOA 2 airfoil studies workshop results ; proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center, Hampton, Virginia, September 23-27, 1988Edward J. Ray
⏱ 4h 18m

CAST-10-2/DOA 2 airfoil studies workshop results ; proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center, Hampton, Virginia, September 23-27, 1988

Edward J. Ray

1989258 pp.
An approach to constrained aerodynamic design with application to airfoilsRichard L. Campbell
⏱ 21m

An approach to constrained aerodynamic design with application to airfoils

Richard L. Campbell

199221 pp.
Computer program to obtain ordinates for NACA airfoilsUnknown Author

Computer program to obtain ordinates for NACA airfoils

Unknown Author

1996No page data
Unsteady aerodynamics of conventional and supercritical airfoilsSanford S. Davis
⏱ 7h 13m

Unsteady aerodynamics of conventional and supercritical airfoils

Sanford S. Davis

1980433 pp.
Mathematical Methods of Airfoil DesignAlexander M. Elizarov
⏱ 4h 52m

Mathematical Methods of Airfoil Design

Alexander M. Elizarov

1997292 pp.
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