Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 /
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| Main Author: | |
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| Corporate Author: | |
| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
[Washington, DC] : [Springfield, Va.] :
National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service],
1992.
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| Series: | NASA technical memorandum
4296. |
| Subjects: |