Numerical investigation on properties of attack angle for an opposing jet thermal protection system

Author:

Lu Hai-Bo,Liu Wei-Qiang

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Cited by 26 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Drag Reduction Mechanism of Array Microslit-Opposed Jets in the Passivation Leading Edge of High-Speed Aircrafts;Journal of Aerospace Engineering;2024-07

2. Angle-of-attack characteristics of opposing jet for improving drag and heat reduction;Physics of Fluids;2024-07-01

3. Simulations of Heat and Drag Reduction of Opposing Jet in Hypersonic Flow;Journal of Spacecraft and Rockets;2023-09

4. Phenomenological Introduction of Standoff Distance of Sonic Ring Impelling Entropy Waves and Aerodynamic Heating of Hypersonic Vehicles;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27

5. Fluidic techniques;Aerodynamic Heating in Supersonic and Hypersonic Flows;2023

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