Low-subsonic static stability and damping derivatives at angles of attack from 0° to 90° for a model with a low-aspect-ratio unswept wing and two different fuselage forebodies / by Peter C. Boisseau.
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| Main Author: | |
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington [D.C.] :
National Aeronautics and Space Administration,
[1959]
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| Series: | NASA memorandum ;
1-22-59L. |
| Subjects: |
Norlin Library - Government Information - US
| Call Number: |
NAS 1.10:1-22-59 L
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| NAS 1.10:1-22-59 L | Available Place a Hold |