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1

Configuration design studies and wind tunnel tests of an energy efficient transport with a high-aspect-ratio supercritical wing /

[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982

Government Document Book

2

Wind tunnel tests of high-lift systems for advanced transports using high-aspect-ratio supercritical wings /

by Allen, John B.
[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982

Government Document Book

3

Wind tunnel tests of high-lift systems for advanced transports using high-aspect-ratio supercritical wings /

by Allen, John B.
[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982

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

Government Document Book

4

Wind tunnel tests of high-lift systems for advanced transports using high-aspect-ratio supercritical wings

by Allen, John B.
[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982

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

Government Document Electronic Book

5

Wind tunnel tests of high-lift systems for advanced transports using high-aspect-ratio supercritical wings

by Allen, John B.
[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1982

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

Government Document Book

6

Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations /

by Brooke, D., Vondrasek, D. V.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Service ; For sale by the National Technical Information Service, 1979

Government Document Book

7

High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft /

by Koch, L. C. (Leland C.), Pagel, L. L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

8

Wing analysis using a transonic potential flow computational method /

by Henne, P. A., Hicks, R. M. (Raymond Morton), 1932-
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

9

Thermal design for areas of interference heating on actively cooled hypersonic aircraft /

by Herring, R. L., Stone, J. E.
Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Office ; For sale by the National Technical Information Service, 1978

Government Document Book

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