Canlyniadau Chwilio am Awdur

1

Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate

gan Blair, A. B.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986

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Government Document Llyfr

2

Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system /

gan Blair, A. B.
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985

Government Document Llyfr

3

Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 c̊lipped-delta-wing orbiter configuration at supersonic mach numbers /

gan Blair, A. B.
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Government Document Llyfr

4

Stability and control characteristics of a monoplanar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86 /

gan Blair, A. B.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Llyfr

5

An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds /

gan Blair, A. B.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979

Government Document Llyfr

6

Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control /

gan Blair, A. B.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Llyfr

7

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers /

gan Blair, A. B.
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 Llyfr

8

Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins /

gan Blair, A. B.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Llyfr

9

Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds /

gan Blair, A. B.
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 Llyfr

10

Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate /

gan Blair, A. B.
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 Llyfr

Pynciau Perthynol