NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
By: Stephen W.D. Wolf, James A. Laub.
Contributors: Laub, James A.; Ames Research Center.
Series: NASA technical memorandum -- 110438.
Publisher: National Aeronautics and Space Administration, Ames Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Moffett Field, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Laminar flow; Supersonic wind tunnels; Wind tunnel tests
Notes: Shipping list no.: 98-0790-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.