An edition of An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street (1966)

An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street

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An analysis of the subsonic flow past symmetr ...
Nash, John F.
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Last edited by Open Library Bot
December 5, 2010 | History
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An edition of An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street (1966)

An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street

by

  • 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
42

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Subjects
Aerodynamic load, Aerofoils

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Edition Availability
Cover of: An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street
An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street
1966, H.M.S.O.
in English
  • Not in Library

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Book Details

Edition Notes

Bibliography: p. 28-30.

Published in
London
Series
[Great Britain] Aeronautical Research Council. Reports and memoranda ;, no. 3436, Reports and memoranda (Aeronautical Research Council (Great Britain)) ;, no. 3436.

Classifications

Dewey Decimal Class
629.13432
Library of Congress
TL526.G7 A4 no. 3436

The Physical Object

Pagination
[1], 42 p.
Number of pages
42

ID Numbers

Open Library
OL5566016M
LCCN
67071202

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