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Keyword [Design mach number]
Result: 1 - 3 | Page: 1 of 1
1.
Investigation Of Hypersonic Inward Turing Inlet With Controlled Mach Number Distribution And Its Integrated Design
2.
Supersonic biplane design via adjoint method
3.
Flow and Acoustics of Jets from Practical Nozzles for High- Performance Military Aircraft
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