完成
发表于 2025-3-27 00:58:25
Time-Resolved Adaptive Direct FEM Simulation of High-Lift Aircraft Configurations, a benchmark problem from the HiLiftPW-3 workshop to compute the flow past a JAXA Standard Model (JSM) aircraft model at realistic Reynolds numbers. The mesh is automatically constructed by the method as part of an adaptive algorithm based on a posteriori error estimation using adjoint techniques. N
Nucleate
发表于 2025-3-27 04:21:30
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AER
发表于 2025-3-27 05:28:07
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NIP
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ligature
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connoisseur
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keloid
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欢呼
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