Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /

Saved in:

Bibliographic Details
Author / Creator:	Stallings, Robert L., author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Description:	1 online resource (45 pages) : illustrations.
Language:	English
Series:	NASA technical paper ; 1789 NASA technical paper ; 1789.
Subject:	Aerothermodynamics. Boundary layer. Supersonic wind tunnels.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914262

Hidden Bibliographic Details
Other authors / contributors:	Lamb, Milton, author. Langley Research Center. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:	Title from title screen (viewed on Aug. 23, 2016). "December 1980." "Performing Organization: NASA Langley Research Center"--Report documentation page. Includes bibliographical references (pages 17-18). Technical paper. National Aeronautics and Space Administration 505-43-23-02 L-14044
Other form:	Print version: Stallings, Robert L. Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 Microfiche version: Stallings, Robert L. Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1789

Similar Items