Suggested Topics within your search.
Showing 1 - 20 results of 53 for search '', query time: 0.28s Refine Results
1
Subsonic and transonic unsteady- and steady-pressure measurements on a rectangular supercritical wing oscillated in pitch /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984

Government Document Book
2
Wing planform effects at supersonic speeds for an advanced fighter configuration /
by Wood, Richard M.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by National Technical Information Service], 1984

Government Document Book
3
Optimization and performance calculation of dual-rotation propellers /
by Davidson, Robert E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
4
Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory /
by Mann, Michael J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984

Government Document Book
5
Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration /
by Murri, Daniel G.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984

Government Document Book
6
Effects of winglets on a first-generation jet transport wing : VII, sideslip effects on winglet loads and selected wing loads at subsonic speeds for a full-span model /
by Meyer, Robert R.
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986

Government Document Book
7
A System for aerodynamic design and analysis of supersonic aircraft.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980

Government Document Book
8
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8° to 90° /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
9
Aeroelastic loads prediction for an arrow wing /
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983

Government Document Book
10
Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters /
by Lamar, John E.
[Washington, D.C.] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1988

Government Document Book
11
Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft /
by White, William L.
Washington, D.C. : [Springfield, Va.] : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
12
Experimental and analytical study of the longitudinal aerodynamic characteristics of analytically and empirically designed strake-wing confirurations at subcritical speeds /
by Lamar, John E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
13
Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls /
by Abel, Irving
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
14
Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
15
Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds /
by Stallings, Robert L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
16
An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect /
by Paulson, John W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
17
Study of supersonic wings employing the attainable leading-edge thrust concept /
by Middleton, W. D. (Wilbur D.), 1931-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
18
An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations /
by Barger, Raymond L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
19
Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /
by Lamb, Milton
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
20
Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 /
by Mann, Michael J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book
Search Tools: Get RSS Feed — Email this Search — Save Search