Similarity solutions for small cross flows in laminar compressible boundary layers / by Ivan E. Beckwith.

The boundary-layer equations for three-dimensional flow have been simplified by the use of a streamline coordinate system and the assumptions of small cross flow and similar profiles. Equations for heat transfer and skin friction for axisymmetric flow are then applicable to three-dimensional flow. S...

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Bibliographic Details
Main Author: Beckwith, Ivan E.
Corporate Authors: Langley Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1961.
Series:NASA technical report ; R-107.
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Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number: NAS 1.12:107
NAS 1.12:107 Available Place a Hold