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

Theoretical stability derivatives of a highly ...
T. Nonweiler, T. Nonweiler
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Last edited by WorkBot
January 24, 2010 | History

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

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Publish Date
Pages
36

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Book Details


Edition Notes

Bibliographical references: p. 27.

Published in
Cranfield, Bedfordshire
Series
College of Aeronautics -- Cranfield. Report ; no. 50

The Physical Object

Pagination
36 p. :
Number of pages
36

ID Numbers

Open Library
OL21040826M

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January 24, 2010 Edited by WorkBot add more information to works
December 11, 2009 Created by WorkBot add works page