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Subjects
Hypersonics, Shock tubesEdition | Availability |
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1
Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel
1965, [Institute for Aerospace Studies]
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Book Details
Edition Notes
Thesis (M.A.Sc.) - University of Toronto, 1965.
Includes bibliographical references.
The Physical Object
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December 11, 2009 | Created by WorkBot | add works page |