Search Results

1

Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 /

by Wood, Richard M.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985

Government Document Book

2

Numerical solutions of Navier-Stokes equations for a Butler wing /

by Abolhassani, Jamshid S.
Norfolk, Va. : [Washington, DC] : [Springfield, Va.] : Old Dominion University Research Foundation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987

Government Document Book

3

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment /

by McMillin, S. Naomi (Susan Naomi)
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990

Government Document Book

4

A review of the planform effects on the low-speed aerodynamic characteristics of triangular and modified triangular wings /

by Razak, Kenneth
Washington, D.C. : National Aeronautics and Space Administration, 1966

Government Document Book

5

Favorable interference effects on maximum lift-drag ratios of half-cone delta-wing configurations at Mach 6.86 /

by Fetterman, David E.
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Virginia 22151], 1965

Government Document Book

6

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment /

by McMillin, S. Naomi (Susan Naomi)
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990

Government Document Book

7

Transonic Navier-Stokes calculations about a 65° delta wing /

by Londenberg, W. Kelly (William Kelly), 1963-
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994

Government Document Book

8

Experimental results of the control of a vortical flow by tangential blowing /

by Wood, N. J.
Stanford, Calif. : [Washington, DC] : [Springfield, Va.] : Stanford University, Dept. of Aeronautics and Astronautics ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1986

Government Document Book

9

Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds /

by Wood, Richard M.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992

Government Document Book

10

Theoretical studies on flapped delta wings /

by Oh, S.
[Moffett Field, Calif.] : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1988

Government Document Book

11

An investigation of asymmetric vortical flows over delta wings with tangential leading-edge blowing at high angles of attack /

by Celik, Zeki Z.
Washington, D.C. : American Institute of Aeronautics and Astronautics, 1990

Conference Proceeding Book

12

Transonic flutter study of a 50.5 c̊ropped-delta wing with two rearward-mounted nacelles /

by Sandford, M. C. (Maynard C.)
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

13

Supersonic aerodynamics of delta wings /

by Wood, Richard M.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1988

Government Document Book

14

Theoretical and experimental longitudinal aerodynamic characteristics of an aspect ratio 0.25 sharp-edge delta wing at subsonic, supersonic, and hypersonic speeds /

by Fox, Charles H.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

15

A second order slender wing theory for wings with leading edge separation in supersonic flow /

by Nenni, Joseph P.
Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971

Government Document Book

16

Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration /

by Fox, Mike C.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993

Book

17

An overview of an experimental demonstration aerotow program /

by Murray, James E., Bowers, Albion H., Lokos, William A., Peters, Todd L., Gera, Joseph
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center, 1998

Government Document Book

18

Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds /

by Erickson, Gary E.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991

Government Document Book

19

Research in computational fluid dynamics : semiannual progress report, reporting period September 1, 1986 - February, 1987 /

by Murman, Earll M., 1942-
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987

Government Document Book

20

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

by Chipman, Richard R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

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