The interaction of a reflected shock wave with the boundary layer in a shock tube.

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Bibliographic Details
Author / Creator:Mark, Herman, 1923-
Imprint:Ithaca, N.Y., Cornell University, Graduate School of Aeronautical Engineering, 1957.
Description:149 . illus. 28 cm.
Language:English
Series:AFOSR-TR-57-345
Subject:
Format: Print Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/4011740
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Notes:"Supported jointly by the Office of Scientific Research, Air Research and Development Command, U.S. Air Force, and the Office of Naval Research.
Issued also as thesis, Cornell University.
ASTIA Document no. AD 132 418.
Bibliography: . 130-131.

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