Analysis of mixing and thrust diagnostics for shock tunnel hot nozzle testing
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999. === Includes bibliographical references. === Transient testing of hot engine exhaust nozzle flows is being pursued to enable cost and time savings of one to two orders of magnitude over steady-state ho...
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| Format: | Others |
| Language: | English |
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Massachusetts Institute of Technology
2009
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| Online Access: | http://hdl.handle.net/1721.1/50074 |