A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow

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A numerical method for calculating the pressu ...
Robert Henry Eldridge
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Last edited by Open Library Bot
December 5, 2010 | History

A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow

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Publish Date
Publisher
H.M.S.O.
Language
English
Pages
49

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Book Details


Edition Notes

Bibliography: p. 21.

Published in
London
Series
Aeronautical Research Council. Reports and memoranda, no. 3535, Reports and memoranda (Aeronautical Research Council (Great Britain)) ;, no. 3535.

Classifications

Dewey Decimal Class
629.13/008 s
Library of Congress
TL526.G7 A4 no. 3535

The Physical Object

Pagination
[1], 49 p.
Number of pages
49

ID Numbers

Open Library
OL4625401M
LCCN
77456512

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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