2022
DOI: 10.1002/ces2.10168
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Mathematical modeling and simulation of porosity on thermomechanical properties of UHTCs under hypersonic conditions

Abstract: Ultrahigh temperature ceramics (UHTCs) were analyzed for their suitability in hypersonic flight conditions using balanced heat equations, transport equation, and finite element modeling technique. Mathematical model was derived on the assumption that the induced porosity follows linear and parabolic solutions of Laplace equation and applied external load mimicking hypersonic conditions with critical heat flux ranging between 7 and 44 MW/m 2 . Simulations were carried out with four different UHTCs combinations … Show more

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Cited by 3 publications
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