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The design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59

The design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59

Master of Science

Bibliographic Details
Main Author: Anderson, Euell Clay
Other Authors: Aerospace Engineering
Format: Others
Language:en_US
Published: Virginia Polytechnic Institute 2016
Subjects:
LD5655.V855 1962.A549
Supersonic wind tunnels > Design
Wind tunnels > Design
Online Access:http://hdl.handle.net/10919/70993
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Internet

http://hdl.handle.net/10919/70993

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