Download New Results in Numerical and Experimental Fluid Mechanics V: by Daniel Reckzeh, Heinz Hansen (auth.), Prof. Dr. Hans-Josef PDF
By Daniel Reckzeh, Heinz Hansen (auth.), Prof. Dr. Hans-Josef Rath, Carsten Holze, Dr. Hans-Joachim Heinemann, Rolf Henke, Professor Dr. Heinz Hönlinger (eds.)
This quantity includes the contributions to the 14. Symposium of the STAB (German Aerospace Aerodynamics Association). during this organization all these German scientists and engineers from universities, learn institutions and are concerned, who're doing examine and undertaking paintings in numerical and experimental fluid mechanics and aerodynamics, in most cases for aerospace yet for different purposes, too. some of the contributions are featuring effects from nationwide and ecu group subsidized initiatives. the amount provides a large evaluate over the continued paintings during this box in Germany, with the subjects being high-aspect ratio wings, low aspect-ratio wings, bluff our bodies, laminar circulate keep watch over and transition, lively circulation keep watch over, hypersonic flows, aeroelasticity, aeroacoustics, mathematical basics/ numerical simulation, actual basics, and facilities.
Read or Download New Results in Numerical and Experimental Fluid Mechanics V: Contributions to the 14th STAB/DGLR Symposium Bremen, Germany 2004 PDF
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Additional resources for New Results in Numerical and Experimental Fluid Mechanics V: Contributions to the 14th STAB/DGLR Symposium Bremen, Germany 2004
The gray tones of the boundaries of areas are related to therespectivecameras. The engine simulator CRUF was mounted in the gap between both flaps. ^ ^n m Figure 3 Position of vortices and relation between radius r and circulation F obtained via approximation with Oseen Vortex (FAM) andfirommoments of vorticity (MOV) as described in Ref. . 696 is depicted in the middle of Fig. 18, a = 12°, 'Ncmf = 3 700/min). 22 H. Vollmers. W. PuffertMeissner, and A. Sdiroder ;l . }»>;! )u . . ;L. y. j. ;•; K'J S>; I D S liWin/s ^.
Then the vorticity of DFS-I- is reduced within two wingspan distances and the wake consists of three vortices: the WTV, the OFV and the counter-rotating HTV. 5 by the merging between the OFV-ONV and the dominant WTV. The analysis of the single vortex strength at the most downstream location reveals weaJcer vortices - 30 C. Bellastrada and C. Breitsamter the W T V and O F V - O N V - for the two DFS t h a n for the baseline configuration. These vortices also present a significant decrease in their viscous core in comparison with t h a t observed for the baseline.
12,2001, pp. 1-9. Analysis of PIV Flow Field Measurements » 21 : Figure 1 The mapping of a pair of dewarped calibration images from both stereo cameras into one image (left side) demonstrates perfect agreement. The upper vector fields (right side) show the view of both cameras. In the lower part the fields are combined and the vectors are within the plane of the light sheet while the gray values indicate the component normal to the light sheet. Figure 2 Investigated areas for 4° (left) and 16° angle of attack seen from down stream.