Transition in hypersonic boundary layers
Transition and turbulence production in a hypersonic boundary layer is investigated in a Mach 6 wind tunnel using Rayleigh-scattering visualization, fast-response pressure measurements, and particle image velocimetry. It is found that the second-mode instability is a key modulator of the transition...
| প্রধান লেখক: | , , , , , , , |
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| বিন্যাস: | প্রবন্ধ |
| ভাষা: | English |
| প্রকাশিত: |
AIP Publishing LLC
2015-10-01
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| মালা: | AIP Advances |
| অনলাইন ব্যবহার করুন: | http://dx.doi.org/10.1063/1.4935019 |