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- W2093704457 abstract "Impact failure of the coating of space shuttle thermal protection tiles was confirmed to occur by a flexure process at low projectile velocities. The critical projectile velocity was measured for a variety of projectile sizes. The same failure process and damage sequence was observed in quasi-static indentation tests. In these tests, the mechanical behavior agreed reasonably well with the elastic model of an infinite plate bonded to a semiinfinite foundation. The model indicates that the critical fracture load could be increased by increasing coating strength, thickness, or foundation stiffness, or by decreasing the Young's modulus of the coating." @default.
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- W2093704457 date "1984-08-01" @default.
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- W2093704457 title "Impact Behavior of Coated Low-Density Bodies" @default.
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- W2093704457 doi "https://doi.org/10.1111/j.1151-2916.1984.tb19171.x" @default.
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