Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65̊ delta wings varying in leading-edge radius and camber [microform] / S. Naomi McMillin [and others]

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Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	McMillin, S. Naomi (Susan Naomi)
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1996]
Series:	NASA technical memorandum ; 4673.
Subjects:	Airplanes > Wings, Triangular. Flow visualization. Camber (Aerofoils) Delta wings. Leading edges. Camber. Pressure ratio.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:4673
NAS 1.15:4673	Restricted Place a Hold