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

Download or Read eBook 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 PDF written by Paul G. Fournier and published by . This book was released on 1959 with total page 24 pages. Available in PDF, EPUB and Kindle.
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
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Total Pages : 24
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ISBN-10 : UIUC:30112106659078
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Rating : 4/5 (78 Downloads)
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Book Synopsis 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 by : Paul G. Fournier

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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 Related Books

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
Language: en
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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

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

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Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90°

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