Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Holger Barnewitz"'
Publikováno v:
AIAA Journal. 55:3304-3317
Nowadays, classical configurations of civil transportation airplanes are well optimized, with further improvements expected to be of the order of a single drag count. To achieve it, the entire airp...
Publikováno v:
17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
Autor:
Norbert Kroll, Antonio Fazzolari, Nicolas R. Gauger, Subhendu Bikash Hazra, Daniel Vollmer, Holger Barnewitz, Joel Brezillon, Richard P. Dwight, Klaus Becker, Volker Schulz
Publikováno v:
Journal of Computational and Applied Mathematics. 203(2):397-411
Within the framework of the German aerospace research program, the CFD project MEGADESIGN was initiated. The main goal of the project is the development of efficient numerical methods for shape design and optimization. In order to meet the requiremen
This volume reports results from the German research initiative MUNA (Management and Minimization of Errors and Uncertainties in Numerical Aerodynamics), which combined development activities of the German Aerospace Center (DLR), German universities
Autor:
Bernd Stickan, Holger Barnewitz
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783642361845
An improved, robust, error reducing CFD-mesh deformation module for the parallel simulation environment FlowSimulator is presented. The mesh deformation method is based on radial basis function interpolation for the surface- and volume- mesh nodes co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::891217f0b7c3e055cf3c8349d32a4607
https://doi.org/10.1007/978-3-642-36185-2_9
https://doi.org/10.1007/978-3-642-36185-2_9
Autor:
Holger Barnewitz
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783642040924
A multi-disciplinary optimisation (MDO) process chain for shape optimisation of a wing including the static deformation has been developed. The objective function, which should be minimized, is equivalent to the total aerodynamic drag force of an air
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8240b43fba926f96baa1f5b1e2c058e6
https://doi.org/10.1007/978-3-642-04093-1_20
https://doi.org/10.1007/978-3-642-04093-1_20