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Theoretical stability derivatives of a highly swept delta wing and slender body combination

College of Aeronautics

Publication Data

Title Theoretical stability derivatives of a highly swept delta wing and slender body combination
Author College of Aeronautics
Publisher College of Aeronautics
Publication date 1951
Language English

Catalogue Data

OBNB ID GB5202155
ISBN 10 n/a
ISBN 13 n/a
Type BibliographicResource, Book
Dewey Classification 629.13236

ISBD

P1053 36p.

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Theoretical stability derivatives of a highly swept delta wing and slender body combination by College of Aeronautics. Published by College of Aeronautics in 1951. Publication and catalogue information, links to buy online and reader comments.

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