A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel [microform] / Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson.

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Bibliographic Details
Main Author:	Lawing, Pierce L.
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Other Authors:	Adcock, Jerry B., Ladson, Charles L.
Format:	Government Document Microfilm Book
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.
Series:	NASA technical paper ; 1752.
Subjects:	Aerodynamics, Transonic. Wind tunnels > Ground simulators > Testing. Low temperature engineering.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.60:1752
NAS 1.60:1752	Available Place a Hold