An edition of Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4 (1970)

Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4

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Heat transfer on a flat plate in continuum to ...
Henry T. Nagamatsu
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Last edited by Open Library Bot
December 5, 2010 | History
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An edition of Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4 (1970)

Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4

by

  • 0 Ratings
  • 0 Want to read
  • 0 Currently reading
  • 0 Have read

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Publish Date
Publisher
National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]
Language
English
Pages
45

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Subjects
Heat, Hypersonic wind tunnels, Rarefied gas dynamics, Transmission

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Cover of: Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4
Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4
1970, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]
in English
  • Not in Library

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Book Details

Edition Notes

Includes bibliographical references.
Cover title.
"Prepared by General Electric Research and Development Center."

Published in
Washington
Series
NASA contractor report, NASA, CR-1692, NASA contractor report ;, NASA CR-1692.

Classifications

Dewey Decimal Class
629.132/3
Library of Congress
TL521.3.C6 A3 no. 1692

The Physical Object

Pagination
xii, 45 p.
Number of pages
45

ID Numbers

Open Library
OL5276059M
LCCN
71610044

Source records

Library of Congress MARC record

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History

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December 5, 2010 Edited by Open Library Bot Added subjects from MARC records.
December 10, 2009 Created by WorkBot add works page