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High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90°

Bernard Spencer

Published: 1959

Total Pages: 34

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High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0 Deg to 90 Deg

Published: 1959

Total Pages: 32

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Static Longitudinal Aerodynamic Characteristics at Transonic Speeds and Angles of Attack Up to 99° of a Reentry Glider Having Folding Wing-tip Panels

Walter B. Olstad

Published: 1961

Total Pages: 36

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An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

Bernard Spencer

Published: 1961

Total Pages: 38

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Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.

AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS

Bernard Spencer

Published: 1960

Total Pages: 32

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An Investigation at Subsonic Speeds of Aerodynamic Charactersitcs at Angles of Attack from -40 to 1000 of a Delta-wing Reentry Configuration Having Folding Wingtip Panels

Bernard Spencer

Published: 1960

Total Pages: 34

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Wind-tunnel Investigation at High Subsonic Speed of the Static Longitudinal Stability Characteristics of a Winged Reentry Vehicle Having a Large Negatively Deflected Flap-type Control Surface

Paul G. Fournier

Published: 1959

Total Pages: 24

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NASA Technical Note

Published: 1963

Total Pages: 902

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Static Longitudinal Aerodynamic Characteristics at Transonic Speeds and Angles of Attack Up to 99 Deg of a Reentry Glider Having Folding Wing-tip Panels

Published: 1961

Total Pages: 36

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Low-speed Longitudinal Aerodynamic Characteristics Associated with a Series of Low-aspect-ration Wings Having Variations in Leading Contour

Bernard Spencer

Published: 1962

Total Pages: 92

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High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90°

High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0 Deg to 90 Deg

Static Longitudinal Aerodynamic Characteristics at Transonic Speeds and Angles of Attack Up to 99° of a Reentry Glider Having Folding Wing-tip Panels

An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS

An Investigation at Subsonic Speeds of Aerodynamic Charactersitcs at Angles of Attack from -40 to 1000 of a Delta-wing Reentry Configuration Having Folding Wingtip Panels

Wind-tunnel Investigation at High Subsonic Speed of the Static Longitudinal Stability Characteristics of a Winged Reentry Vehicle Having a Large Negatively Deflected Flap-type Control Surface

NASA Technical Note

Static Longitudinal Aerodynamic Characteristics at Transonic Speeds and Angles of Attack Up to 99 Deg of a Reentry Glider Having Folding Wing-tip Panels

Low-speed Longitudinal Aerodynamic Characteristics Associated with a Series of Low-aspect-ration Wings Having Variations in Leading Contour

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