A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer /

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Bibliographic Details
Author / Creator:	Jackson, Charlie M., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, March 1969.
Description:	1 online resource (65 pages) : illustrations.
Language:	English
Series:	NASA technical note ; TN D-5046 NASA technical note ; D-5046.
Subject:	Drag (Aerodynamics) Boundary layer. Boundary layer. Drag (Aerodynamics)
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12675081

Hidden Bibliographic Details
Other authors / contributors:	Smith-Taylor, Rudeen, author. United States. National Aeronautics and Space Administration, issuing body. Langley Research Center.
Notes:	"March 1969." Includes bibliographical references (pages 48-49). Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 4, 2020).
Other form:	Print version: Jackson, Charlie M. Method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer
GPO item no.:	0830-H-13 (online)
Govt.docs classification:	NAS 1.14:D-5046

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