Investigation on the Effects of Atwood Number on the Combustion Performance of Hydrogen-Oxygen Supersonic Mixing Layer
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Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-33-6060-0_3
Reference31 articles.
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5. Goncharov VN (2002) Analytical model of nonlinear, single-mode, classical Rayleigh-Taylor instability at arbitrary Atwood numbers. Phys Rev Lett 88(13):134502. https://doi.org/10.1103/PhysRevLett.88.134502
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