Comparison of flight pressure measurements with wind-tunnel data and theory for the forward fuselage of the X-15 airplane at Mach numbers from 0.8 to 6.0 /
Jon S. Pyle.

Description

Main Author

Pyle, Jon S.

Related Names

Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : 1964.

Subjects

X-15 (Rocket aircraft) > X-15 (Rocket aircraft) / Design and construction.

Physical Description

29 p. : ill. ; 27 cm.

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