Zobrazeno 1 - 10
of 1 538
pro vyhledávání: '"Schröder Wolfgang"'
Publikováno v:
Acta Acustica, Vol 7, p 5 (2023)
The accuracy of two direct coupled two-step CFD/CAA methods is discussed. For the flow field either a finite-volume (FV) method for the solution of the Navier–Stokes equations or a lattice Boltzmann (LB) method is coupled to a discontinuous Galerki
Externí odkaz:
https://doaj.org/article/cf176b0786de421bb1200feaf2b82dfa
Autor:
Lambertz Rolf, Chang De-hua, Hickethier Tilman, Bagheri Mahsa, Leers Jessica M., Bruns Christiane J., Schröder Wolfgang
Publikováno v:
Innovative Surgical Sciences, Vol 4, Iss 3, Pp 85-90 (2019)
Postoperative chylothorax is a serious complication after transthoracic esophagectomy, and is associated with major morbidity due to dehydration and malnutrition. For patients with high-output fistula, re-thoracotomy with ligation of the thoracic duc
Externí odkaz:
https://doaj.org/article/54405645644f428fa7d4ba57636266ba
In the age of globalization, commercial aviation plays a central role in maintaining our international connectivity by providing fast air transport services for passengers and freight. However, the upper limit of the aircraft flight envelope, i.e., i
Externí odkaz:
http://arxiv.org/abs/2401.08894
Autor:
Rottmayer, Jan, Özkaya, Emre, Satcunanathan, Sutharsan, Zhou, Beckett Y., Aehle, Max, Gauger, Nicolas R., Meinke, Matthias, Schröder, Wolfgang, Pullin, Shaun
Broadband noise reduction is a significant problem in aerospace and industrial applications. Specifically, the noise generated from the trailing edge of an airfoil poses a challenging problem with various proposed solutions. This study investigates t
Externí odkaz:
http://arxiv.org/abs/2301.13047
The transonic flow around the OAT15A airfoil is computed at buffet conditions, i.e., freestream Mach number $Ma_\infty = 0.73$, chord-based freestream Reynolds number $Re_c = 2\cdot10^6$, and angle of attack $\alpha = 3.5^\circ$ using wall-modeled LE
Externí odkaz:
http://arxiv.org/abs/2301.05889