Subsonic tests in free molecule flow on impact tube pressure probes having a wide range of tube lengths at angles of attack up to 90 ̊ /

Bibliographic Details
Main Author:	Hughes, Peter C. (Peter Carlisle), 1940-
Corporate Authors:	University of Toronto. Institute for Aerospace Studies, Air Force Cambridge Research Center (U.S.)
Format:	Book
Language:	English
Published:	[Toronto] : [University of Toronto, Institute for Aerospace Studies], [1965]
Series:	UTIAS technical note ; no. 92.
Subjects:	Molecular dynamics. Tubes > Aerodynamics > Testing. Wind tunnels.

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