Titlebook: New Results in Numerical and Experimental Fluid Mechanics IV; Contributions to the Christian Breitsamter,Boris Laschka,Reinhard Hilbi Confe

Oscillate

Application of fast and advanced CFD for high-lift configuration design taskswith a Navier-Stokes method, trailing edge layout studies with a quasi-3D method and prediction of Reynolds number and engine installation effects with 3Dviscous-Panel, 3D-Euler- and 3D-Navier-Stokes methods.

FRET

bleach

Pressure and heat flux measurements at the surface of an asymmetric cone at Mach number 4.6 in ISL’so create a cone asymmetry. With these models differential interferometry flow visualisations, surface pressure and heat transfer measurements were performed at Mach number 4.6 and 7 km altitude atmospheric conditions at the ISL’s shock tunnel STB to examine the resulting flow around the asymmetric cone model.

蜿蜒而流

Control of Flow around Bluff Bodies by Passive Wake Ventilation numbers, reaching up to 66% for spheres. High drag reductions were also found for elongated bluff bodies at angle of incidence 5 deg and 10 deg. At zero angle of incidence the ventilation effect decreases with increasing fineness ratio. Pitching moment was enhanced by wake ventilation.

angiography

彎彎曲曲

Canary

Numerical Investigation of the Flow Around Different Slat Tracks on a Swept High Lift Wing Segment For the aircraft track only a minor lift change is found, but also a 20% drag increase. Based on the outcome of the present investigations, the major impact on the lift is caused by the downstream shift of the stagnation line in the vicinity of the junction of the model track and the fixed wing.

BILL

BYRE

locus-ceruleus

dresses the gap that has existed between acquisitions on the one hand and social responsibility and sustainability on the other, for an integrative perspective on enacting M&As and achieving the triple people-planet-profits bottom line..978-3-030-05478-6