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1
Nonlinear aerodynamics and the design of wing tips final report, year 1 ... covering the period April 1, 1990 to March 31, 1991 /
by Kroo, Ilan
Stanford, Calif. : [Washington, D.C. : Dept. of Aeronautics and Astronautics, Stanford University ; National Aeronautics and Space Administration, 1991

Government Document Book
2
Numerical prediction of transition of the F-16 wing at supersonic speeds
by Cummings, Russell M.
San Luis Obispo, CA : [Washington, DC : Springfield, Va. : California Polytechnic State University ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1993

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Government Document Book
3
Determination of aerodynamic sensitivity coefficients for wings in transonic flow Leland A. Carlson and Hersham M. El-Banna.
by Carlson, Leland A.
College Station, Tex. : [Washington, DC : Springfield, Va.? : Aerospace Engineering Dept., Texas A&M University ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1992

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Government Document Book
4
Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis semiannual progress report, January 1, 1988 - June 30, 1988 /
by Carlson, Leland A.
College Station, Tex. : Texas Engineering Experiment Station, 1988

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Government Document Book
5
High speed transport cruise drag by Leonard Roberts.
by Roberts, L.
Stanford, CA : Joint Institute for Aeronautics and Acoustics, , 1992

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Government Document Book
6
Nonlinear aerodynamics and the design of wing tips final report, year 2 ... covering the period 1 April 1991 to 31 March 1992 /
by Kroo, Ilan
Stanford, Calif. : Dept. of Aeronautics and Astronautics, [Stanford University, 1992

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Government Document Book
7
An analytical approach to grid sensitivity analysis for NACA four-digit wing sections
by Sadrehaghighi, I.
Norfolk, Va. : [Springfield, Va.? : Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University ; National Technical Information Service [distributor], 1992

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Government Document Book
8
Computation of three-dimensional effects on two dimensional wings
by Cummings, Russell M.
San Luis Obispo, CA : [Washington, DC : Springfield, Va.? : California Polytechnic State University ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1992

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Government Document Book
9
Adjoint methods for aerodynamic wing design semi-annual progress report /
by Grossman, Bernie, b. 1885
[Washington, DC : Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1993

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Government Document Book
10
Effect of wing flexibility on the experimental characteristics of an oblique wing /
by Hopkins, Edward J.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; for sale by the National Technical Information Service, 1977

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Government Document Book
11
Effects of winglets on the drag of a low-aspect-ratio configuration /
by Smith, Leigh Ann
Hampton, Va. : National Aeronautics and Space Administration, 1996

Book
12
Flight-measured wing surface pressures and loads for the X-15 airplane at mach numbers from 1.2 to 6.0 /
by Pyle, Jon S.
Washington, D.C. : National Aeronautics and Space Administration, 1965

Government Document Book
13
Experimental study of complex vortex interactions in the wake of high aspect ratio wings : final report on NASA grant NAG-1-1816 /
by Savas, Ömer
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997

Government Document Book
14
An analytical approach to grid sensitivity analysis for NACA four-digit wing sections /
by Sadrehaghighi, I.
Norfolk, Va. : [Springfield, Va.?] : Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University ; [National Technical Information Service [distributor], 1992

Government Document Book
15
Low-speed static wind-tunnel investigation of a half-span fuselage and variable-sweep pressure wing model /
by Lamar, John E.
Washington, D.C. : National Aeronautics and Space Administration, 1971

Government Document Book
16
The FC-1D : the profitable alternative Flying Circus Commercial Aviation Group : 1993/1994 AIAA/Lockheed Corporation Team Aircraft Design Competition /
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994

Government Document Book
17
Residual strength and crack propagation tests on C-130 airplane center wings with service-imposed fatigue damage /
by Snider, H. Lawrence
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1972

Government Document Book
18
Analysis of wing slipstream flow interaction /
by Jameson, Antony, 1934-
Washington, D.C. : National Aeronautics and Space Administration, 1970

Government Document Book
19
Aerodynamic characteristics of a large-scale V/STOL transport model with tandem lift fans mounted at mid-semispan of the wing /
by Dickinson, Stanley O.
Washington, D.C. : Springfield, VA : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971

Government Document Book
20
Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis : semiannual progress report, January 1, 1988 - June 30, 1988 /
by Carlson, Leland A.
College Station, Tex. : Texas Engineering Experiment Station, 1988

Government Document Book
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