Formulas pertinent to the calculation of flow-field effects at supersonic speeds due to wing thickness / by Kenneth Margolis and Miriam H. Elliott.

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Bibliographic Details
Main Author:	Margolis, Kenneth
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Elliott, Miriam H.
Format:	Government Document Book
Language:	English
Published:	Washington [D.C.] : National Aeronautics and Space Administration, [1959]
Series:	NASA memorandum ; 4-3-59L.
Subjects:	Air flow > Mathematical models. Aerodynamics, Supersonic. Airplanes > Wings.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.10:4-3-59 L
NAS 1.10:4-3-59 L	Available Place a Hold