Titlebook: New Results in Numerical and Experimental Fluid Mechanics V; Contributions to the Hans-Josef Rath,Carsten Holze,Heinz H?nlinger Conference

作業(yè)

書目名稱New Results in Numerical and Experimental Fluid Mechanics V影響因子(影響力)




書目名稱New Results in Numerical and Experimental Fluid Mechanics V影響因子(影響力)學科排名




書目名稱New Results in Numerical and Experimental Fluid Mechanics V網(wǎng)絡公開度




書目名稱New Results in Numerical and Experimental Fluid Mechanics V網(wǎng)絡公開度學科排名




書目名稱New Results in Numerical and Experimental Fluid Mechanics V被引頻次




書目名稱New Results in Numerical and Experimental Fluid Mechanics V被引頻次學科排名




書目名稱New Results in Numerical and Experimental Fluid Mechanics V年度引用




書目名稱New Results in Numerical and Experimental Fluid Mechanics V年度引用學科排名




書目名稱New Results in Numerical and Experimental Fluid Mechanics V讀者反饋




書目名稱New Results in Numerical and Experimental Fluid Mechanics V讀者反饋學科排名

inculpate

接合

slipped-disk

correspondent

Application of the PSP Technique in Low Speed Wind Tunnelsipped with two propeller simulators driven by pressurized air. The great challenge was to compensate the influence of the warm and cold air pipes which are guided inside the wing, creating large temperature differences on the models surface. The PSP (pressure sensitive paint) measurements were carri

填滿

monochromatic

cunning

Aerodynamic Optimisation of a Flying Wing Transport Aircraftord length opfimisation. The applied finite volume flow solver is the DLR code FLOWer. The methods are described and results for a flying wing configuration are presented. The paper represents parts of DLR’s contribution to the aerodynamics work package of the VELA project, supported by European Com

分開

使長胖

Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver test case is presented and compared to other numerical results. Having put the numerical method’s validity into evidence, the unsteady flow induced by an oscillating flap is investigated for a Fighter Type Delta Wing.