Search Results

1

Exploratory investigation of the effect of porous surfaces on hypersonic turbulent boundary layers /

by Watson, Ralph D.
[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

2

Characteristics of Mach 10 transitional and turbulent boundary layers /

by Watson, Ralph D.
[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

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

4

Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data /

by Powers, Sheryll Goecke
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Office, 1978

Government Document Book

5

Simulation of turbulent wall pressure /

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

Government Document Book

6

Turbulent boundary layers over nonstationary plane boundaries /

by Roper, Alan T., Gentry, Garl L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Office, 1978

Government Document Book

7

Transitional boundary-layer solutions using a mixing-length and a two-equation turbulence model /

by Anderson, E. Clay, Wilcox, David C.
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

Representation of turbulent shear stress by a product of mean velocity differences /

by Braun, Willis H.
Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977

Government Document Book

9

Progress in turbulence modeling for complex flow fields including effects of compressibility /

by Wilcox, David C.
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

10

Finite-difference solution of the compressible stability eigenvalue problem /

by Malik, Mujeeb R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book

11

A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) /

by Dash, Sanford M., Pergament, Harold S.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Service ; For sale by the National Technical Information Service, 1978

Government Document Book

12

A visual investigation of turbulence in stagnation flow about a circular cylinder /

by Sadeh, Willy Z., Brauer, Herbert 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

13

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

14

Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9 /

by Deveikis, William D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1978

Government Document Book

15

Turbulent-flow separation criteria for overexpanded supersonic nozzles /

by Morrisette, E. Leon, Goldberg, Theodore 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

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