Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves

Mazhul, I. I.

doi:10.1134/s0869864320040046

Thermophys. Aeromech.

2020

DOI: 10.1134/s0869864320040046

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Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves

I. I. Mazhul

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Cited by 4 publications

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Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves

Cited by 4 publications

References 10 publications

Condensation properties of water vapor under different back pressures in nozzle

Condensation properties of water vapor under different back pressures in nozzle

Energy separation and CO2 nonequilibrium condensation effects in the pressure recovery process of hydrogen-rich fuel purification and decarburization

Numerical simulation of a three-dimensional flow in a channel with interaction of a plane shock wave and a longitudinally ribbed surface

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