The formulation of an influence-coefficient method for determining static aeroelastic effects

and its application to a slender aircraft in symmetric flight at M = 2.2

The formulation of an influence-coefficient m ...
A. S. Taylor, A. S. Taylor
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Last edited by ImportBot
July 17, 2022 | History

The formulation of an influence-coefficient method for determining static aeroelastic effects

and its application to a slender aircraft in symmetric flight at M = 2.2

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Publish Date
Publisher
H.M.S.O.
Language
English
Pages
50

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Book Details


Edition Notes

Bibliography: p. 26.
Cover title.

Published in
London
Series
Aeronautical Research Council. Reports and memoranda,, no. 3573, Reports and memoranda (Aeronautical Research Council (Great Britain)) ;, no. 3573.

Classifications

Dewey Decimal Class
629.13/008 s, 629.132/362
Library of Congress
TL526.G7 A4 no. 3573, TL574.A37 A4 no. 3573

The Physical Object

Pagination
[1], 36 p., 37-50 p. of 36 illus.
Number of pages
50

ID Numbers

Open Library
OL5324176M
ISBN 10
0114702322
LCCN
72176900
OCLC/WorldCat
388918
Goodreads
3537956

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History

Download catalog record: RDF / JSON
July 17, 2022 Edited by ImportBot import existing book
December 5, 2010 Edited by Open Library Bot Added subjects from MARC records.
December 10, 2009 Created by WorkBot add works page