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