CFD Analysis of radiative heat loading on hypervelocity re- entry vehicles

机译：超高速再入飞行器辐射热负荷的CFD分析

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《16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference》|2009年|1-7|共7页
会议地点 Bremen(DE)
作者
S. Karl; M. Lambert;
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作者单位

German Aerospace Center (DLR), GÃ¶ttingen, Germany;

German Aerospace Center (DLR), GÃ¶ttingen, Germany;

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会议组织
原文格式 PDF
正文语种 eng
中图分类各类型航空器;
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1. Computational Analysis of Radiative Heat Loading on Hypervelocity Reentry Vehicles [J] . Karl Sebastian, Potter Daniel, Lambert Markus, Journal of Spacecraft and Rockets . 2015,第1期

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2. Radiative Heating on the After-Body of Martian Entry Vehicles [J] . Brandis A. M., Saunders D. A., Johnston C. O., Journal of Thermophysics and Heat Transfer . 2020,第1期

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3. CFD Analysis of the Effect of Surface Contour of Nose Cone of a Space Vehicle on the Thermal Field during Re-Entry [J] . K.V Sreenivas Rao, P. Sujan, H.S. Sachin Applied Mechanics and Materials . 2018,第期

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4. CFD Analysis of radiative heat loading on hypervelocity re- entry vehicles [C] . S. Karl, M. Lambert American Institute of Aeronautics and Astronautics/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference . 2009

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5. Time-accurate conjugate CFD analysis of a jet-impingement configuration with sudden changes in heating and cooling loads. [D] . Lee, Chien-Shing. 2014

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6. CFD analysis on heat and flow characteristics of double helically coiled tube heat exchanger handling MWCNT/water nanofluids [O] . P.C. Mukesh Kumar, M. Chandrasekar 2019

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7. Hypervelocity Aeroheating Measurements in Wake of Mars Mission Entry Vehicle [O] . Perkins John N., Hollis Brian R. 1995

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8. Stagnation Point Heat Transfer in High Enthalpy Gas Flows. Part II: Shock Layer Radiative Emission During Hypervelocity Re-Entry [R] . Nerem, R. M. 1964

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CFD Analysis of radiative heat loading on hypervelocity re- entry vehicles

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