Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 /
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
U.S. National Aeronautics and Space Administration ;
1976.
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| Series: | NASA technical memorandum ;
NASA TM X-3313. |
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| Item Description: | Cover title. |
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| Physical Description: | 1 unnumbered page, 205 pages : illustrations ; 27 cm. |
| Bibliography: | Bibliography: page 18. |