Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /

Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /

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Bibliographic Details
Author / Creator:	Nowak, Robert J., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1985.
Description:	1 online resource (87 pages) : illustrations.
Language:	English
Series:	NASA/TP ; 2345 NASA technical paper ; 2345.
Subject:	Angle of attack (Aerodynamics) Noses (Aircraft) Reynolds number. Aerothermodynamics. Aerothermodynamics. Angle of attack (Aerodynamics) Noses (Aircraft) Reynolds number.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11618373

Hidden Bibliographic Details
Other authors / contributors:	Albertson, Cindy W., author. Hunt, L. Roane (Lewis Roane), author. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:	"January 1985." Prepared at Langley Research Center. Includes bibliographical references (pages 19-21). Technical paper. NASA Langley Research Center 506-51 -23-03 L-15729 Description based on online resource, PDF version; title from title page (NASA, viewed June 12, 2018).
Other form:	Print version: Nowak, Robert J Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes Microfiche: Nowak, Robert J Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:2345

Description
Item Description:	"January 1985." Prepared at Langley Research Center.
Physical Description:	1 online resource (87 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 19-21).