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

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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
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Total Pages : 32
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ISBN-10 : NASA:31769000459803
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Book Synopsis 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 by : Bernard Spencer

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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 Related Books

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
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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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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.
Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings
Language: en
Pages: 52

Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings

Authors:
Categories:
Type: BOOK - Published: 1963 - Publisher:

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Keywords Index to U.S. Government Technical Reports
Language: en
Pages: 88

Keywords Index to U.S. Government Technical Reports

Authors:
Categories: Government publications
Type: BOOK - Published: 1963-06-15 - Publisher:

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