A Computational Approach to Heat Transfer and Ablation in Space Capsule Insulation

Author:

Saboohi Zoheir,Razmjooei Mohammad,Karimi Nima,Golmakani Atousa

Publisher

Elsevier BV

Reference31 articles.

1. Extending Inverse Heat Conduction Method to Estimate Flight Trajectory of a Reentry Capsule;V Tahmasbi;AUT Journal of Mechanical Engineering,2020

2. Novel Engineering Methodology for Decoupled Aerothermal Analysis of Hypersonic Atmospheric Entry Flows;J M Cooper;Journal of Spacecraft and Rockets,2023

3. Aero-heating modelling on the ablative noses during flight trajectory;M M Doustdar;Aircraft Engineering and Aerospace Technology,2018

4. Engineering aerodynamic heating method for hypersonic flow;C J Riley;Journal of Spacecraft and Rockets,1992

5. A new method for solution of viscous shock-layer equations;S Noori;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2010

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