Titlebook: New Results in Numerical and Experimental Fluid Mechanics VII; Contributions to the Andreas Dillmann,Gerd Heller,Wolfgang Schr?der Conferen

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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

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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

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