Computational Analysis of Zel'dovich-von Neumann-Doering (ZND) Detonation
The Transient Inlet Concept (TIC) involves transient aerodynamics and wave interactions with the objective of producing turbulence, compression and flow in ducted engines at low subsonic speeds. This concept relies on the generation and control of multiple detonation waves issuing from different ?st...
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| Format: | Others |
| Language: | English |
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2010
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| Online Access: | http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-395 |