Conjugate flow-thermal analysis of a hypersonic reentry vehicle in the rarefied flow regime-Reference-Cited by-同舟云学术

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Conjugate flow-thermal analysis of a hypersonic reentry vehicle in the rarefied flow regime

Published:2022-02 Issue:2 Volume:34 Page:026107
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Appar Ahilan¹^ORCID,Kumar Rakesh¹^ORCID,Naspoori Srujan K.¹

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur, Uttar Pradesh 208016, India

Funder

Indian Space Research Organisation

Science and Engineering Research Board

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

https://aip.scitation.org/doi/pdf/10.1063/5.0082783

Reference59 articles.

1. Ablation and radiation coupled viscous hypersonic shock layers.

2. Laminar-to-turbulent transitions over an ablating reentry capsule

3. A method for calculating intense injection from surfaces of blunt bodies entering planetary atmospheres at hypersonic velocities

4. Computation of weakly ionized hypersonic flows in thermochemical nonequilibrium

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2. Numerical study of gas–surface interface effects due to transpiration in a hypersonic flow over a blunt body;Physics of Fluids;2024-01-01

3. The Investigation of Fluid-Thermal-Catalysis-Radiation Coupling Scheme of Conjugate Heat Transfer for Heterogeneous Recombination Reaction Process;2024

4. Conjugate Heat Transfer in High-Speed External Flows: A Review;Journal of Thermophysics and Heat Transfer;2023-10

5. Self-similar analysis of gas dynamics for van der Waals gas in slipping flow after normal shock wave;Physics of Fluids;2023-02-01

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