Effects of cone angle, base flare angle, and corner radius on Mach 3.0 aerodynamic characteristics of large-angle cones /

Effects of cone angle, base flare angle, and corner radius on Mach 3.0 aerodynamic characteristics of large-angle cones /

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Bibliographic Details
Author / Creator:	Deveikis, William D., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, March 1969.
Description:	1 online resource (45 pages) : illustrations.
Language:	English
Series:	NASA technical note ; TN D-5048 NASA technical note ; D-5048.
Subject:	Space vehicles -- Aerodynamics. Wind tunnels. Cone -- Aerodynamics. Cone -- Aerodynamics. Space vehicles -- Aerodynamics. Wind tunnels.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12675084

Hidden Bibliographic Details
Other authors / contributors:	Sawyer, James Wayne, 1941- author. United States. National Aeronautics and Space Administration, issuing body. Langley Research Center.
Notes:	"March 1969." Includes bibliographical references (page 17). Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 4, 2020).
Other form:	Print version: Deveikis, William D. Effects of cone angle, base flare angle, and corner radius on Mach 3.0 aerodynamic characteristics of large-angle cones
GPO item no.:	0830-H-13 (online)
Govt.docs classification:	NAS 1.14:D-5048

Description
Item Description:	"March 1969."
Physical Description:	1 online resource (45 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 17).