Showing 1 - 20 results of 33 for search 'Mineck, Raymond E.', query time: 0.11s Refine Results
1
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
2
Reynolds number effects on the performance of lateral control devices
by Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 2000

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document Book
3
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques
by 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 Book
4
Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic tunnel /
by 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 Book
5
Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft /
by Mineck, Raymond E.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book
6
Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel /
by 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 Book
7
Study of potential aerodynamic benefits from spanwise blowing at wingtip /
by Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from the National Technical Information Service, 1995

Book
8
Reynolds number effects on the performance of lateral control devices /
by Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 2000

Government Document Book
9
Tail contribution to the directional aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with a tail rotor /
by Mineck, Raymond E.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book
10
Effect of full-chord porosity on aerodynamic characteristics of the NACA 0012 airfoil /
by Mineck, Raymond E.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from the National Technical Information Service, 1996

Book
11
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques /
by Mineck, Raymond E.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Government Document Book
12
Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /
by Mineck, Raymond E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
13
Study of potential aerodynamic benefits from spanwise blowing at wingtip /
by Mineck, Raymond E.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995

Government Document Book
14
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
15
High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by Mineck, Raymond E.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987

Government Document Book
16
Assessment of potential aerodynamic benefits from spanwise blowing at the wing tip /
by Mineck, Raymond E.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1992

Government Document Book
17
Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel /
by 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.
Book
18
Reynolds number effects on the performance of lateral control devices /
by Mineck, Raymond E.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2000

Government Document Book
19
Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section /
by 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 Book
20
Aerodynamic characteristics of a 1/6-scale powered model of the rotor systems research aircraft /
by Mineck, Raymond E., Freeman, Carl E.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book
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