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

NASA Ames Laminar Flow Supersonic Wind Tunnel ...
Stephen W. D. Wolf
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Last edited by WorkBot
January 19, 2010 | History

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

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Cover of: NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
1997, National Aeronautics and Space Administration, Ames Research Center, National Technical Information Service, distributor
Microform in English
Cover of: NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
1997, National Aeronautics and Space Administration, Ames Research Center, National Technical Information Service, distributor
Microform in English

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Book Details


Edition Notes

Shipping list no.: 98-0790-M.

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

Published in
Moffett Field, Calif, [Springfield, Va
Series
NASA technical memorandum -- 110438.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL15498180M

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January 19, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page