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Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets
To aim at design requirements of high lift-to-drag ratio as well as high volumetric efficiency of next generation hypersonic airplanes, a body-wing-blending configuration with double flanking air inlets layout...
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Open AccessAerodynamic optimization and evaluation for the three-dimensional afterbody/nozzle integrated configuration of hypersonic vehicles
The optimization of 2D expansion lines and key parameters of three-dimensional configurations was carried out under simulated conditions of Mach 6.5 and a flight altitude of 25 km for an integrated configurati...
