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- W2023961662 abstract "A three-dimensional flux-based thermal analysis method has been developed and its capability is demonstrated by predicting the transient nonlinear temperature response of a swept cowl leading edge subjected to intense three-dimensional aerodynamic heating. The predicted temperature response from the transient thermal analysis is used in a linear elastic structural analysis to determine thermal stresses. Predicted thermal stresses are compared with those obtained from a two-dimensional analysis which represents conditions along the chord where maximum heating occurs. Results indicate a need for a three-dimensional analysis to predict accurately the leading edge thermal stress response." @default.
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- W2023961662 date "1992-01-01" @default.
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- W2023961662 title "Three-dimensional thermal structural analysis of a swept cowl leading edge subjected to skewed shock-shock interference heating" @default.
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