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 MARC Bot
October 9, 2020 | 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 / OPDS | Wikipedia citation
October 9, 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