An edition of Experiments in aircraft roll-yaw control using forebody tangential blowing (1997)

Experiments in aircraft roll-yaw control using forebody tangential blowing

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Experiments in aircraft roll-yaw control usin ...
Nelson Pedreiro.
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January 21, 2010 | History
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An edition of Experiments in aircraft roll-yaw control using forebody tangential blowing (1997)

Experiments in aircraft roll-yaw control using forebody tangential blowing

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Publish Date
Publisher
Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, Joint Institute for Aeronautics and Acoustics, Stanford University, National Technical Information Service, distributor
Language
English

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Subjects
Aircraft control, Control simulation, Vortices, Roll, Mathematical models, Yaw, Forebodies, Angle of attack, Tangential blowing, Flight control, Flow visualization, Wind tunnel models, Aerodynamic characteristics, Wind tunnel tests, Computerized simulation

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Cover of: Experiments in aircraft roll-yaw control using forebody tangential blowing
Experiments in aircraft roll-yaw control using forebody tangential blowing
1997, Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, Joint Institute for Aeronautics and Acoustics, Stanford University, National Technical Information Service, distributor
Microform in English
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Book Details

Edition Notes

Shipping list no.: 99-0433.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 2 microfiches.

Published in
[Stanford, Calif.], [Springfield, Va
Series
JIAA TR -- 120., [NASA contractor report] -- NASA/CR-208349., NASA contractor report -- NASA CR-208349.
Other Titles
Experiments in aircraft roll yaw control using forebody tangential blowing.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL15545010M

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January 21, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page