Showing 1 - 7 results of 7 for search 'Spahr, J. Richard', query time: 0.02s
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1
Effect of tail surfaces on the base drag of a body of revolution at Mach numbers of 1.5 and 2.0 / by Spahr, J. Richard
Published 1951Call Number: Loading…
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2
Theoretical investigation of the effects of configuration changes on the center-of-pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transoni... by Spahr, J. Richard
Published 1957Call Number: Loading…
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3
Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles / by Spahr, J. Richard
Published 1958Call Number: Loading…
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4
Measurements in flight of the stability, lateral control, and stalling characteristics of an airplane equipped with full-span zap flaps and spoiler-type ailerons / by Spahr, J. Richard
Published 1943Call Number: Loading…
Located: Loading…Government Document Book Loading… -
5
Measurements in flight of the lateral-control characteristics of an airplane equipped with full-span zap flaps and simple circular-arc-type aiilerons / by Spahr, J. Richard
Published 1944Call Number: Loading…
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6
Theoretical prediction of the effects of vortex flows on the loading, forces, and moments of slender aircraft / by Spahr, J. Richard
Published 1961Call Number: Loading…
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7
Lateral-control characteristics of various spoiler arrangements as measured in flight / by Spahr, J. Richard
Published 1947Call Number: Loading…
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Related Subjects
Airplanes
Control
Flight testing
Aerodynamics
Aerodynamics, Supersonic
Ailerons
Flaps (Airplanes)
Spoilers (Airplanes)
Stability of airplanes, Lateral
Wind tunnel testing
Wings
Airframes
Angle of attack (Aerodynamics)
Body of revolution
Boundary layer
Drag (Aerodynamics)
Fuselage
Mathematical analysis
Pitching (Aerodynamics)
Rolling (Aerodynamics)
Tail surfaces
Tails
Trailing edges (Aerodynamics)
Vortex flaps