A Reduced Order Model of an External Compression Supersonic Inlet.
The research contained in this thesis was performed in order to model the external compression axisymmetric inlet portion of a supersonic jet engine in a way that captures the effects of a full 3-D CFD model while maintaining the quickness of a lower dimensional model. This was accomplished by first...
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Full Text (via ProQuest) |
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| Format: | Thesis eBook |
| Language: | English |
| Published: |
Ann Arbor :
ProQuest Dissertations & Theses,
2016.
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