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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