Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0 /

Saved in:

Bibliographic Details
Author / Creator:	McGhee, Robert J., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, March 1969.
Description:	1 online resource (39 pages) : illustrations.
Language:	English
Series:	NASA technical note ; D-5030 NASA technical note ; D-5030.
Subject:	Aerodynamics, Supersonic. Supersonic nozzles. Mach number. Aerodynamics, Supersonic. Mach number. Supersonic nozzles.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12674951

Hidden Bibliographic Details
Other authors / contributors:	Martin, James A., author. United States. National Aeronautics and Space Administration, issuing body. Langley Research Center.
Notes:	"March 1969." Includes bibliographical references (page 11). Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 16, 2020).
Other form:	Print version: McGhee, Robert J Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0
GPO item no.:	0830-H-13 (online)
Govt.docs classification:	NAS 1.14:D-5030

Similar Items