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1
Aeronautical research augmentor wing system : agreement between the United States of America and Canada amending and extending the agreement of October 10, 1970, as extended effected by exchange of notes signed at Ottawa August 14 and 19, 1981.
Washington, D.C. : Dept. of State : For sale by the Supt. of Docs., U.S. G.P.O., 1983

Government Document Book
2
Aeronautical research : augmentor wing system : agreement between the United States of America and Canada, extending the agreement of October 19 and November 10, 1970, as extended, effected by exchange of notes, signed at Ottawa, May 31 and July 18, 1977.
[Washington] : Dept. of State : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1979

Government Document Book
3
Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line
by Mineck, Raymond E.
[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; National Technical Information Service, distributor], 1993

Government Document Book
4
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
5
Space shuttle pinhole formation mechanism studies
by Jacobson, Nathan S.
[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1998

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Government Document Book
6
Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing
[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1999

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Government Document Book
7
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
8
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
9
A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration
by Rao, Dhanvada M.
Hampton, Va. : [Springfield, Va.? : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service [distributor], 1992

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Government Document Book
10
Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design
by Carlson, Harry W.
[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

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Government Document Book
11
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
12
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
13
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

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
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

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document Book
15
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

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document Book
16
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
17
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
18
Wing theory in supersonic flow /
by Carafoli, Elie
Oxford, New York : Pergamon Press, 1969
[First edition].

Book
19
Wing-with-stores flutter.
Neuilly-sur-Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1975

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Conference Proceeding Book
20
On the prediction of aerodynamic loads on osillating wings in transonic flow /
by Tijdeman, H.
[Neuilly-sur-Seine, France] : North Atlantic Treaty Organization : Advisory Group for Aerospace Research and Development, 1974

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Book
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