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- W4317693648 abstract "Rapidly predicting aerodynamic loads is a fundamental challenge in the early phases of conceptual and preliminary design of high speed systems. This work discusses the impact of using a CFD-based kriging surrogate approach for an axisymmetric vehicle configuration for Mach numbers from 0.60 to 3.95. Both standard and hierarchical kriging CFD surrogates for aerodynamic coefficients are compared to wind tunnel results from an open source NASA-designed configuration (NASA-TM-213541). The impact of varying both fidelity and amount of training data on the overall model is assessed so as to provide guidance on trade-offs when considering how to best implement CFD-based surrogates." @default.
- W4317693648 created "2023-01-22" @default.
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- W4317693648 date "2023-01-19" @default.
- W4317693648 modified "2023-09-27" @default.
- W4317693648 title "CFD-Based Kriging Surrogate Models Compared to Axisymmetric Missile Concept From Mach 0.60 to 3.95" @default.
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- W4317693648 doi "https://doi.org/10.2514/6.2023-2278" @default.
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