Aeroacoustics of the bifurcated 2D supersonic inlet
An investigation was performed to determine the aerodynamic and acoustic performance of the bifurcated 2D supersonic inlet during takeoff and approach flight conditions, and to compare these results indirectly to those of the axisymmetric supersonic inlet. The comparison is not direct since the cent...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/45084 http://scholar.lib.vt.edu/theses/available/etd-10072005-094852/ |