An edition of Aerodynamic characteristics of the 10-percent-thick NASA supercritical airfoil 33 designed for a normal-force coefficient of 0.7 (1981)

Aerodynamic characteristics of the 10-percent-thick NASA supercritical airfoil 33 designed for a normal-force coefficient of 0.7.

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Aerodynamic characteristics of the 10-percent ...
Charles D. Harris, Charles D. ...
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Last edited by WorkBot
December 10, 2009 | History
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An edition of Aerodynamic characteristics of the 10-percent-thick NASA supercritical airfoil 33 designed for a normal-force coefficient of 0.7 (1981)

Aerodynamic characteristics of the 10-percent-thick NASA supercritical airfoil 33 designed for a normal-force coefficient of 0.7.

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Publish Date
Publisher
NASA Langley Research Center
Language
English

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Edition Availability
Cover of: Aerodynamic characteristics of the 10-percent-thick NASA supercritical airfoil 33 designed for a normal-force coefficient of 0.7.
Aerodynamic characteristics of the 10-percent-thick NASA supercritical airfoil 33 designed for a normal-force coefficient of 0.7.
1981, NASA Langley Research Center
in English

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Book Details

Edition Notes

Published in
Hampton, VA
Series
Technical memoranda / National Aeronautics and Space Administration -- TM X-72711

ID Numbers

Open Library
OL13839687M

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