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Published in 2019 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2019.03.023
Abstract: Abstract The effect of the penetration mode on the thermal protection system by opposing jet is studied in this paper. The results show that the opposing jet not only pushes the bow shock away from…
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Keywords:
thermal protection;
jet;
opposing jet;
penetration mode ... See more keywords
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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2020.03.004
Abstract: Abstract The drag reduction characteristics play an important role in the supersonic vehicle design phase. According to two drag reduction schemes, the opposing jet and the upstream energy deposition have aroused the widespread interest of…
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Keywords:
energy deposition;
reduction;
opposing jet;
drag reduction ... See more keywords
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Published in 2019 at "Chinese Journal of Aeronautics"
DOI: 10.1016/j.cja.2019.03.015
Abstract: Abstract In this paper, a Non-Ablative Thermal Protection System (NATPS) with the spiked body and the opposing jet combined configuration is proposed to reduce the aerodynamic heating of the hypersonic vehicle, and the coupled fluid-thermal…
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Keywords:
system;
opposing jet;
body;
spiked body ... See more keywords
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1
Published in 2017 at "Journal of Aerospace Engineering"
DOI: 10.1061/(asce)as.1943-5525.0000659
Abstract: AbstractAn equal polygon opposing jet can withstand huge wave drag and serious aerodynamic heating in hypersonic flow conditions. The opposing jet is able to change the flow field structure, and then it improves the aerodynamic…
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Keywords:
equal polygon;
polygon opposing;
jet;
opposing jet ... See more keywords
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3
Published in 2023 at "Journal of Spacecraft and Rockets"
DOI: 10.2514/1.a35696
Abstract: To reduce aerodynamic heat and drag, and thus improve the speed of hypersonic vehicles, opposing jet technology has become a research focus because of its excellent heat and drag reduction effect. In this paper, Navier–Stokes…
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Keywords:
opposing jet;
reduction;
jet;
heat drag ... See more keywords