Experimental Investigation of the Effects of Aerospike Geometry on Aerodynamic Drag and Heat Transfer Rates for a Blunt Body Configuration at Hypersonic Mach Numbers
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Portico
Cited by 13 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. 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
2. Mechanical techniques (spike);Aerodynamic Heating in Supersonic and Hypersonic Flows;2023
3. Supersonic flow investigation of a drag reducing conical spike on a hemispherically blunted nose body;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-11-26
4. Study of Drag Reduction on a Hypersonic Vehicle Using Aerospike;Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics;2022-06-24
5. Numerical investigation of aerospike semi-cone angle and a small bump on the spike stem in reducing the aerodynamic drag and heating of spiked blunt-body: New correlations for drag and surface temperature;Physics of Fluids;2021-11
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