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An Analysis of Combined Radiation-Conductive Heat Transfer During the Destruction of Porous Carbon-Ceramic Composite Material of the Thermal Protection Shield
| Authors: Prosuntsov P.V., Barinov D.Y. | Published: 13.12.2020 |
| Published in issue: #12(729)/2020 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: mathematical model, descent module, thermal protection, radiation- conductive heat transfer |
