A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer /
Saved in:
Author / Creator: | Jackson, Charlie M., author. |
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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: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12675081 |
Other authors / contributors: | Smith-Taylor, Rudeen, author. United States. National Aeronautics and Space Administration, issuing body. Langley Research Center. |
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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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