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.
Subject:Boundary layer.
Shock waves.
Format: Print Book
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Hidden Bibliographic Details
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.

Crerar, Lower Level, Dewey Collection

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Call Number: 532.51 W701
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