Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained During Demonstration Flights to a Mach Number of 1.20

Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained During Demonstration Flights to a Mach Number of 1.20
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Total Pages : 23
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ISBN-10 : OCLC:715440314
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Book Synopsis Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained During Demonstration Flights to a Mach Number of 1.20 by : Donald R. Bellman

Download or read book Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained During Demonstration Flights to a Mach Number of 1.20 written by Donald R. Bellman and published by . This book was released on 1954 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lift and drag data were obtained during the manufacturer and Air Force demonstration flights of the Douglas X-3 airplane. The data covered the Mach number range from 0.82 to 1.20 with considerable variation in lift.

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