An edition of Numerical integration methods for supersonic wings in steady and oscillatory motion (1955)

Numerical integration methods for supersonic wings in steady and oscillatory motion

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Numerical integration methods for supersonic ...
Bernard Etkin
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February 7, 2010 | History
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An edition of Numerical integration methods for supersonic wings in steady and oscillatory motion (1955)

Numerical integration methods for supersonic wings in steady and oscillatory motion

by

  • 0 Ratings
  • 0 Want to read
  • 0 Currently reading
  • 0 Have read

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Publish Date
Publisher
Institute of Aerophysics
Pages
37

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Subjects
Supersonic flow, Flutter, Wings

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Edition Availability
Cover of: Numerical integration methods for supersonic wings in steady and oscillatory motion
Numerical integration methods for supersonic wings in steady and oscillatory motion
1955, Institute of Aerophysics
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Book Details

Edition Notes

Includes bibliographical references.

Published in
[Downsview, Ont.]
Series
UTIA report -- no.36

The Physical Object

Pagination
37 p. :
Number of pages
37

ID Numbers

Open Library
OL20897574M

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February 7, 2010 Edited by WorkBot add more information to works
December 10, 2009 Created by WorkBot add works page