Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration

Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration
Author: Gerald V. Foster
Publisher:
Total Pages: 28
Release: 1959
Genre: Aerodynamics, Supersonic
ISBN:
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Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration
Language: en
Pages: 28

Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration

Authors: Gerald V. Foster
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1959 - Publisher:

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Exploratory Investigation at Mach Number of 2.01 of Longitudinal Stability and Control Characteristics of Winged Reentry Configuration [with List of References]
Language: en
Pages: 21

Exploratory Investigation at Mach Number of 2.01 of Longitudinal Stability and Control Characteristics of Winged Reentry Configuration [with List of References]

Authors:
Categories: Space vehicles
Type: BOOK - Published: 1959 - Publisher:

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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
Language: en
Pages: 40

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

Authors: Bernard Spencer
Categories: Aerodynamics
Type: BOOK - Published: 1961 - Publisher:

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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
Language: en
Pages: 32

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

Authors: Bernard Spencer
Categories: Air flow
Type: BOOK - Published: 1960 - Publisher:

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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
Language: en
Pages: 34

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

Authors: Bernard Spencer
Categories: Air flow
Type: BOOK - Published: 1960 - Publisher:

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