Some finite difference solutions of the laminar compressible boundary layer showing the effects of upstream transpiration cooling / by John T. Howe.

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Bibliographic Details
Main Author:	Howe, John T.
Corporate Authors:	Ames Research Center, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	Washington [DC] : National Aeronautics and Space Administration, 1959.
Series:	NASA memorandum ; 2-26-59A.
Subjects:	Laminar boundary layer > Mathematical models. Cooling > Mathematical models. Fluid mechanics > Mathematical models.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.10:2-26-59 A
NAS 1.10:2-26-59 A	Available Place a Hold