Showing 1 - 12 results of 12 for search 'Penland, Jim A.', query time: 0.12s Refine Results
1
Maximum lift-drag-ratio characteristics of rectangular and delta wings at Mach 6.9 /
by Penland, Jim A.
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Virginia 22151], 1965

Government Document Book
2
Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results /
by Penland, Jim A.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1997

Government Document Book
3
Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels /
by Penland, Jim A.
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
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 s̊wept double-delta wing at Mach numbers from 1.50 to 2.86 /
by Penland, Jim A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
5
Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 s̊wept delta wing /
by Penland, Jim A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
6
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 s̊wept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /
by Penland, Jim A.
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
7
Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° /
by Penland, Jim A.
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1957

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document Book
8
Aerodynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle /
by Penland, Jim A.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service, distributor], 1985

Government Document Book
9
Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6 /
by Penland, Jim A.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1987

Government Document Book
10
Low-speed aerodynamic characteristics of a lifting-body hypersonic research aircraft configuration /
by Penland, Jim A., Creel, Theodore R.
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Government Document Book
11
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 s̊wept double-delta wing at Mach number 0.2 /
by Penland, Jim A., Creel, Theodore R., Dillon, James 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
12
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /
by Penland, Jim A., Hallissy, James B., Dillon, James L.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979

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