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: |
| Item Description: | Cover title. "March 1959." |
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| Physical Description: | 25 pages : illustrations ; 26 cm. |
| Bibliography: | Includes bibliographical references (page 9) |