Отображение 1 - 20 результаты of 35 для поиска 'Mineck, Raymond E.', время запроса: 0.09сек. Отмена результатов
1
Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line
по 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 ‌
2
Reynolds number effects on the performance of lateral control devices
по Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 2000

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Government Document ‌
3
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques
по Mineck, Raymond E.
[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

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document ‌
4
Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel /
по Mineck, Raymond E.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990

Government Document ‌
5
Study of potential aerodynamic benefits from spanwise blowing at wingtip /
по Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from the National Technical Information Service, 1995

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6
Reynolds number effects on the performance of lateral control devices /
по Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 2000

Government Document ‌
7
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques /
по Mineck, Raymond E.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Government Document ‌
8
Study of potential aerodynamic benefits from spanwise blowing at wingtip /
по Mineck, Raymond E.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995

Government Document ‌
9
Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line /
по 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 ‌
10
Assessment of potential aerodynamic benefits from spanwise blowing at the wing tip /
по Mineck, Raymond E.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1992

Government Document ‌
11
Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel /
по Mineck, Raymond E.
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
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12
Reynolds number effects on the performance of lateral control devices /
по Mineck, Raymond E.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2000

Government Document ‌
13
Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section /
по Mineck, Raymond E.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document ‌
14
Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft /
по Mineck, Raymond E.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document ‌
15
Tail contribution to the directional aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with a tail rotor /
по Mineck, Raymond E.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document ‌
16
Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel /
по Mineck, Raymond E.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1989

Government Document ‌
17
Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section /
по Mineck, Raymond E.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987

Government Document ‌
18
High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /
по Mineck, Raymond E.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987

Government Document ‌
19
Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /
по Mineck, Raymond E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document ‌
20
Effect of full-chord porosity on aerodynamic characteristics of the NACA 0012 airfoil /
по Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from the National Technical Information Service, 1996

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