Low-speed wind-tunnel tests on an unswept wing-fuselage model of aspect ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream

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Low-speed wind-tunnel tests on an unswept win ...
J. A. Lawford
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Last edited by MARC Bot
October 5, 2020 | History

Low-speed wind-tunnel tests on an unswept wing-fuselage model of aspect ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream

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

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Publish Date
Language
English
Pages
35

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Book Details


Edition Notes

Includes bibliographical references.
Cover title.

Published in
London
Series
Aeronautical Research Council. Current papers,, no. 1108, Current papers (Aeronautical Research Council (Great Britain)) ;, no. 1108.

Classifications

Dewey Decimal Class
629.13 s, 629.134/52
Library of Congress
TL507 .G77 no. 1108

The Physical Object

Pagination
21, [35] p.
Number of pages
35

ID Numbers

Open Library
OL5772586M
LCCN
71534499

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History

Download catalog record: RDF / JSON / OPDS | Wikipedia citation
October 5, 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