The dynamic stability derivatives of a slender wing

a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4

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The dynamic stability derivatives of a slende ...
K. J. Turner
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Last edited by MARC Bot
October 4, 2020 | History

The dynamic stability derivatives of a slender wing

a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4

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

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Publish Date
Publisher
H.M.S.O.
Language
English
Pages
43

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Book Details


Edition Notes

Bibliography: p. 38-43.

Published in
London
Series
Aeronautical Research Council. Current papers, no. 995, Current papers (Aeronautical Research Council (Great Britain)) ;, no. 995.

Classifications

Dewey Decimal Class
629.13/008 s
Library of Congress
TL507 .G77 no. 995

The Physical Object

Pagination
[1], 43 p.
Number of pages
43

ID Numbers

Open Library
OL5725603M
LCCN
70459082

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History

Download catalog record: RDF / JSON / OPDS | Wikipedia citation
October 4, 2020 Edited by MARC Bot import existing book
December 14, 2009 Edited by WorkBot link works
April 1, 2008 Created by an anonymous user Imported from Scriblio MARC record