Coupled fluid-thermal investigation on non-ablative thermal protection system with spiked body and opposing jet combined configuration
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference27 articles.
1. Thermal protection system gap analysis using a loosely coupled fluid-structural thermal numerical method;Huang;Acta Astronaut,2018
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3. Fluid-thermal analysis of aerodynamic heating over spiked blunt body configurations;Qin;Acta Astronaut,2017
4. Drag reduction investigation for hypersonic lifting-body vehicles with aerospike and long penetration mode counterflowing jet;Deng;Aerosp Sci Technol,2018
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1. Flow-thermal coupled investigation on hypersonic spike-jet with channel;Acta Astronautica;2024-10
2. Numerical study on drag and heat flux reduction induced by a counterflowing jet for rarefied hypersonic flow over a blunt body;Physics of Fluids;2024-04-01
3. Comparison of single and multi-coolant axial jets on the temperature reduction of nose cone with multiple-row disk;Results in Engineering;2023-12
4. Heated wind-tunnel experiments and numerical investigations onhypersonic blunt cone aerodynamic heating;Acta Astronautica;2022-08
5. Coupled surface-volume pyrolysis effects of carbon-phenolic resin composites under hyperthermal non-equilibrium flows;Physics of Fluids;2022-06
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