NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 / Stephen W.D. Wolf, James A. Laub.

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Bibliographic Details
Online Access:	Online Access
Main Authors:	Wolf, Stephen W. D. (Author), Laub, James A. (Author)
Other title:	NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 degree cone at Mach 1.6.
Format:	Government Document eBook
Language:	English
Published:	Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, March 1997.
Series:	NASA technical memorandum ; 110438.
Subjects:	Laminar flow. Supersonic wind tunnels. Wind tunnel tests.

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Call Number:	NAS 1.15:110438
NAS 1.15:110438	Available