NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /

Bibliographic Details

Main Authors:	Wolf, Stephen W. D. (Author), Laub, James A. (Author)
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.
Online Access:	https://purl.fdlp.gov/GPO/gpo78568