Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry

Download or Read eBook Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry PDF written by George M. Ware and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle.
Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry
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Total Pages : 20
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ISBN-10 : UIUC:30112105148057
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Rating : 4/5 (57 Downloads)
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Book Synopsis Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry by : George M. Ware

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Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry Related Books

Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry
Language: en
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Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry

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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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