Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow

part 1-theoretical results for the wing thickness case

Pressure distributions on planar and crucifor ...
Y. Y. Chan, Y. Y. Chan
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Last edited by Open Library Bot
December 5, 2010 | History

Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow

part 1-theoretical results for the wing thickness case

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Publish Date
Language
English
Pages
82

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Book Details


Edition Notes

Includes bibliographical references.

Published in
[Melbourne]
Series
Dept. of Supply. Australian Aeronautical Research Committee. Report ACA-69

Classifications

Library of Congress
TL507 .A8 no. 69

The Physical Object

Pagination
82 p.
Number of pages
82

ID Numbers

Open Library
OL5516356M
LCCN
73490390

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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