Search Results

1

Nonlinear lift and pressure distribution of slender conical bodies with strakes at low speeds /

by Levinsky, E. S.
Washington, D.C. : National Aeronautics and Space Administration, 1968

Government Document Book

2

Analytical and experimental investigation of circulation control by means of a turbulent Coanda jet /

by Levinsky, E. S.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

3

The Effect of lift on entry corridor depth and guidance requirements for the return lunar flight /

by Wong, Thomas J.
Washington, DC : U.S. G.P.O., 1961

Government Document Book

4

Lifting-surface theory for calculating the loading induced on a wing by a flap /

by Johnson, Wayne, 1946-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

5

Aerodynamic influence coefficient method using singularity splines /

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

Government Document Book

6

Evaluation of advanced lift concepts and potential fuel conservation for short-haul aircraft /

by Sweet, H. S.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

7

Wind-tunnel investigation of a large 35 s̊wept-wing jet transport model with an external-flow jet-augmented double-slotted flap /

by Aoyagi, Kiyoshi
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971

Government Document Book

8

Effects of forward contour modification on the aerodynamic characteristics of the NACA 64₁-212 airfoil section /

by Hicks, R. M. (Raymond Morton), 1932-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

9

Large-scale static investigation of circulation-control-wing concepts applied to upper-surface-blowing aircraft /

[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987

Government Document Book

10

STOL technology; a conference held at NASA Ames Research Center, Moffet Field, California, October 17-19, 1972.

Washington, Scientific and Technical Information Office, National Aeronautics and Space Administration, 1972

Government Document Book

11

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

12

Leading-edge slat optimization for maximum airfoil lift /

by Olson, Lawrence E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1979

Government Document Book

13

Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

by Wick, Bradford H.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

14

Effects of body shape on the aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 /

by Nelms, Walter P.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

15

Large-scale wind tunnel investigation to improve the low-speed longitudinal stability at high lift of a supersonic transport with variable-sweep wings /

by Cook, Anthony M.
Washington, D.C. : National Aeronautics and Space Administration, 1969

Government Document Book

16

Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport /

by Cook, Anthony M.
Washington, D.C. : National Aeronautics and Space Administration, 1968

Government Document Book

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