Using of ANSYS CFX software for calculate the characteristics of aviation combat aircraft powerplants to increase flight safety

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The article presents the main results of the research on improving the design and of supersonic air inlets characteristics of combat aircraft complexes of the fourth generation. Constructive activities aimed on improving the flight safety and the take-off and landing characteristics of combat aircraft are offered for practical recommendations

Combat aircraft of the fourth generation, supersonic air inlet, intensity of the vortex flow, foreign bodies, numerical method of research, airborne protective device, sub window feed

Короткий адрес: https://sciup.org/148201273

IDR: 148201273

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