Author:
Leonov V. V.,Zarubin V. S.
Reference20 articles.
1. Avduevskiy V.S., Galitseyskiy B.M., Glebov G.A. Osnovy teploperedachi v aviatsionnoy i raketno- kosmicheskoy tekhnike [Fundamentals of Heat Transfer in Aviation and Rocket and Space Technology]. Mashinostroenie, Moscow, 1992, 528 p.
2. Duffa G. Ablative thermal protection systems modeling. American Institute of Aeronautics and Astronautics, Inc., 2013, 431 p.
3. Surzhikov S. Dependence of the Parameters of Shock Layer for Super-Orbital Space Vehicles at Increasing of Entry Velocity. In 55th AIAA Aerospace Sciences Meeting, 2017, p. 1147.
4. A hybrid model of hypersonic flow
5. Leonov V. V. and Grishko D.A. Estimates of the Trajectory Parameters and Thermal Loads for a Ballistic Capsule Returning from the Moon with Multiple Dives into the Earth Atmosphere. Journal of Engineering and Applied Sciences, 14(6), 2019, pp. 1775–1780.
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