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1

An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect /

by Paulson, John W.
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

2

Natural laminar flow experiments on modern airplane surfaces /

by Holmes, Bruce J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984

Government Document Book

3

Analysis of nonplanar wing-tip-mounted lifting surfaces on low-speed airplanes /

by Van Dam, C. P. (Cornelis P.), 1954-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book

4

Subsonic panel method for designing wing surfaces from pressure distribution /

by Bristow, D. R.
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book

5

Development of an efficient procedure for calculating the aerodynamic effects of planform variation /

by Mercer, J. E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book

6

Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement /

by Henderson, William P.
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

7

Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 t̊o 90 /̊

by Mulcay, William
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

8

Induced drag ideal efficiency factor of arbitrary lateral-vertical wing forms /

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

Government Document Book

9

Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings /

by Capone, Francis J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book

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