Search Results

1

Operational manual for two-dimensional transonic code TSFOIL /

by Stahara, Stephen S.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

2

Correlation of laser velocimeter measurements over a wing with results of two prediction techniques /

Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

3

Water-tunnel experiments on an oscillating airfoil at RE = 21,000 /

by McAlister, Kenneth W., Carr, Lawrence W.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

4

An experimental evaluation of the application of the Kirchhoff formulation for sound radiation fron an oscillating airfoil /

by Brooks, Thomas F.
[Washington] : Springfield, Va. : National Aeronoautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977

Government Document Book

5

Analysis of strong-interaction dynamic stall for laminar flow on airfoils /

by Gibeling, H. J., Shamroth, S. J., Eiseman, P. R.
Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

6

Airfoil design by numerical optimization using a minicomputer /

by Hicks, R. M. (Raymond Morton), 1932-, Szelazek, C. A.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

7

Flight evaluation of the transonic stability and control charcteristics of an airplane incorporating a supercritical wing /

by Matheny, Neil W., Gatlin, Donald H.
Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

8

Comparison of elastic and elastic-plastic structural analyses for cooled turbine blade airfoils /

by Kaufman, Albert, 1928-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book

9

The status of analytical preparation for two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel /

by Lewis, M. C.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1984

Government Document Book

10

Erosion/corrosion of turbine airfoil materials in the high-velocity effluent of a pressurized fulidized coal combustor /

by Zellers, Glenn R., Rowe, Anne P., Lowell, Carl E.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

11

High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /

by Mineck, Raymond E.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987

Government Document Book

12

Simple turbulence models and their application to boundary layer separation /

by Wadcock, Alan
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book

13

Experimental investigation of three helicopter rotor airfoils designed analytically /

by Bingham, Gene J., Noonan, Kevin W.
Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979

Government Document Book

14

Effects of upper surface modification on the aerodynamic characteristics of the NACA 632-215 airfoil section /

by Hicks, R. M. (Raymond Morton), 1932-, Shairer, Edward T.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979

Government Document Book

15

Influence of surface static-pressure orifices on boundary-layer transition /

by Somers, Dan M.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982

Government Document Book

16

Low-speed aerodynamic characteristics of a 16-percent thick variable-geometry airfoil designed for general aviation applications /

by Barnwell, Richard W., Noonan, Kevin W., McGhee, Robert J.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

17

Approximation concepts for numerical airfoil optimization /

by Vanderplaats, Garret N.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979

Government Document Book

18

Application of shock tubes to transonic airfoil testing at high Reynolds number /

by Cook, William John, 1929-
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

19

An experimental investigation of gapwise periodicity and unsteady aerodynamic response in an oscillating cascade /

by Carta, F. O. (Franklin O.)
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1982

Government Document Book

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