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1
Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
di 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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Documento governativo Libro
2
Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system /
di Blair, A. B.
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985

Documento governativo Libro
3
Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 c̊lipped-delta-wing orbiter configuration at supersonic mach numbers /
di Blair, A. B.
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Documento governativo Libro
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 /
di Blair, A. B.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Documento governativo Libro
5
An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds /
di 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

Documento governativo Libro
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 /
di 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

Documento governativo Libro
7
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers /
di 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

Documento governativo Libro
8
Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins /
di 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

Documento governativo Libro
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 /
di 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

Documento governativo Libro
10
Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate /
di 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

Documento governativo Libro
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