Titlebook: New Results in Numerical and Experimental Fluid Mechanics VI; Contributions to the Cameron Tropea,Suad Jakirlic,Heinz H?nlinger Conference

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Studies on Tailplane Stall for a Generic Transport Aircraft Wind Tunnel Model configuration is numerically optimised to obtain large Reynolds numbers at the horizontal tailplane in a wind tunnel of limited size. It consists of a fuselage, a detachable horizontal tailplane and a tip-truncated wing, that mounts the model to the turntables of the closed test section. The wing w

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A New Actuator Disk Model for the TAU Code and Application to a Sailplaine with a Folding Enginees a discontinous pressure jump to the flow. The topology of the grid maintains fluxes conservative through the disk. The load of the disk is calculated by time averaging the sectional load of a rotating blade. The sectional load is calculated with the blade element theory for a propeller of a sailp