Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane /
| Main Authors: | , |
|---|---|
| Corporate Author: | |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington, D.C.] :
National Aeronautics and Space Administration, Scientific and Technical Information Division,
December 1987.
|
| Series: | NASA technical memorandum ;
4009. |
| Subjects: | |
| Online Access: | https://purl.fdlp.gov/GPO/gpo76171 |
| Item Description: | "December 1987"--Report documentation page. "Performing organization: NASA Langley Research Center"Report documentation page. |
|---|---|
| Physical Description: | 1 online resource (vii, 80 pages) : illustrations. |
| Bibliography: | Includes bibliographical references (pages 18-19). |