Abstract
Hydrodynamic methods based on the injection of a coolant gas into the boundary layer—the intense heating zone—through porous surfaces are widely used to protect the head part of flight vehicles and surfaces of power plants against high-enthalpy and chemically aggressive gas flows.
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Yakimov, A.S. (2018). Active Thermal Protection. In: Thermal Protection Modeling of Hypersonic Flying Apparatus. Innovation and Discovery in Russian Science and Engineering. Springer, Cham. https://doi.org/10.1007/978-3-319-78217-1_2
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DOI: https://doi.org/10.1007/978-3-319-78217-1_2
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