Numerical Investigation of Gas-Surface Interactions due to Ablation of High-Speed Vehicles-Reference-Cited by-同舟云学术

Numerical Investigation of Gas-Surface Interactions due to Ablation of High-Speed Vehicles

Published:2016-05 Issue:3 Volume:53 Page:538-548
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Kumar Rakesh¹

Affiliation:

1. Indian Institute of Technology Kanpur, Uttar Pradesh 208 016, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33433

Reference22 articles.

1. Ablative Thermal Protection Systems Modeling

2. KendallR.RindalR.BartlettE. “Thermochemical Ablation,” AIAA Paper 1965-0642, 1965.

3. KooJ.HoD.EzekoyeO. “A Review of Numerical and Experimental Chatacterization of Thermal Protection Materials—Part I. Numerical Modeling,” AIAA Paper 2006-4936, 2006.

4. KooJ.HoD.BrunsM.EzekoyeO. “A Review of Numerical and Experimental Chatacterization of Thermal Protection Materials—Part II. Properties Characterization,” AIAA Paper 2007-2131, 2007.

5. SwannR.PittmanC. “Numerical Analysis of the Transient Response of Advanced Thermal Protection Systems for Atmospheric Entry,” NASA Rept. TN-D-1370, 1962.

Cited by 11 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. The effects of energy accommodation of reflected gas molecules on flow structures during expired spacecraft reentry;Computers & Fluids;2024-08

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. Modeling continuous laser ablation of glass fiber-reinforced epoxy resin plate with two-dimensional finite element;Journal of Thermal Analysis and Calorimetry;2023-05-11

4. Rarefied gas effects on hypersonic flow over a transpiration-cooled flat plate;Physics of Fluids;2023-01-01

5. Conjugate flow-thermal analysis of a hypersonic reentry vehicle in the rarefied flow regime;Physics of Fluids;2022-02