Optimization of Plenum for Control of Boundary Layer-Shock Interaction in Supersonic Inlet.
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- Journal of Polytechnic, 2024, v. 27, n. 4, p. 1269, doi. 10.2339/politeknik.1247300
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Works matching DE "TURBOJET plane engine air intakes"
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Numerical investigation of the performance of Heller type cooling towers in different arrangements from the perspective of air intake flow rate.
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- Mechanics & Industry, 2015, v. 16, n. 6, p. 1, doi. 10.1051/meca/2015020
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