eucalyptus
发表于 2025-4-1 03:06:22
Automatic Transition Prediction for Three-Dimensional Aircraft Configurations Using the DLR , Codeien-Schlichting and cross-flow instabilities were coupled for the automatic prediction of laminar-turbulent transition on general aircraft configurations during the ongoing flow computation. The procedure is applied to a three-dimensional wing-body configuration and the sensitivity of the coupled sy
panorama
发表于 2025-4-1 09:58:48
Numerical Simulation of the Elastic and Trimmed Aircraftpled with a procedure to account for the interaction between fluid and structure. The trim algorithm is based on a Newton method with a discretized Jacobian. It incorporates the six degreesof- freedom (DoF) flight-mechanics equations and thereby enables to compute different trimmed states. The fluid
我们的面粉
发表于 2025-4-1 13:58:58
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Focus-Words
发表于 2025-4-1 14:22:34
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OATH
发表于 2025-4-1 20:55:28
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