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Отображение 1 - 20 результаты of 41 для поиска '', время запроса: 0.16сек. Отмена результатов
1
Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).
Washington, D.C : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document ‌
2
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 ‌
3
Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /
по Capone, Francis J.
[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 ‌
4
Aerodynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle /
по 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 ‌
5
Pressure data for four analytically defined arrow wings in supersonic flow /
по Townsend, James C. (James Courtland), 1938-
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 ‌
6
Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /
по Carlson, Harry W.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document ‌
7
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
по Pittman, Jimmy L.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document ‌
8
Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /
по Berrier, Bobby L.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document ‌
9
Supersonic wings with significant leading-edge thrust at cruise /
по Robins, A. Warner
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 ‌
10
Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls /
по Corlett, William A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document ‌
11
Some observations on a new numerical method for solving the Navier-Stokes equations /
по Kumar, Ajay, 1946-
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 ‌
12
Velocity field of a round jet in a cross flow for various jet injection angles and velocity ratios /
по Fearn, Richard L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document ‌
13
Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /
по 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 ‌
14
Steady and nonsteady supersonic turbulent afterbody flow /
по Yoshikawa, Kenneth K.
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 ‌
15
Numerical simulation of steady supersonic viscous flow /
по Schiff, Lewis B.
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 ‌
16
Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 /
по Shrout, Barrett 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 ‌
17
A finite difference solution for the propagation of sound in near sonic flows /
по Hariharan, S. I.
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 ‌
18
Experimental investigation of leading-edge thrust at supersonic speeds /
по Wood, Richard M.
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 ‌
19
Study of supersonic wings employing the attainable leading-edge thrust concept /
по 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 ‌
20
A wing concept for supersonic maneuvering /
по Mason, William H. (William Henry), 1947-
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 ‌
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