Zobrazeno 1 - 10
of 39
pro vyhledávání: '"Norbert Kroll"'
The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as presented and discussed by internationally recognized researchers at the Closing Symposium of the DFG Research Unit FOR 1066. Reliable simulations of flow
Autor:
Krzysztof J. Fidkowski, Georg May, H. T. Huynh, Zhijian J Wang, Rémi Abgrall, Doru Caraeni, Bram van Leer, Per-Olof Persson, Andrew Cary, Herman Deconinck, Koen Hillewaert, Francesco Bassi, Miguel R. Visbal, Norbert Kroll, Ralf Hartmann
Publikováno v:
International Journal for Numerical Methods in Fluids. 72:811-845
After several years of planning, the 1st International Workshop on High-Order CFD Methods was successfully held in Nashville, Tennessee, on January 7-8, 2012, just before the 50th Aerospace Sciences Meeting. The American Institute of Aeronautics and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dde8b191d2c16487592bbeb18edf2148
https://doi.org/10.1002/fld.3767
https://doi.org/10.1002/fld.3767
The book describes the main findings of the EU-funded project IDIHOM (Industrialization of High-Order Methods – A Top-Down Approach). The goal of this project was the improvement, utilization and demonstration of innovative higher-order simulation
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f3b808af1a14831a5d407c4923445f52
A straightforward implicit smoothing method implemented in several codes solving the Reynolds-averaged Navier–Stokes equations is the lower–upper symmetric Gauss–Seidel method. It was proposed several years ago and is attractive to implement be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::acf59a36c7540a06f88c8bab45ea6c66
https://doi.org/10.2514/1.j053367
https://doi.org/10.2514/1.j053367
Autor:
Koen Hillewaert, Norbert Kroll, F. Bassi, Tobias Leicht, Ch. Hirsch, C. Johnston, K.A. Soerensen
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
In aeronautical industry numerical flow simulation has become a key element in the aerodynamic design process. However, in order to meet the ambitious goals for air traffic of the next decades, significant investment in enhancing the capabilities and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a867bccb761c2934c3c694fe654eadfd
https://doi.org/10.2514/6.2015-0293
https://doi.org/10.2514/6.2015-0293
Autor:
Norbert Kroll
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319128856
In aeronautical industry numerical flow simulation has become a key element in the aerodynamic design process. However, in order to meet the ambitious goals for air traffic of the next decades, significant investment in enhancing the capabilities and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b4cb1cb675f99acb1dbeb1c6178105c7
https://doi.org/10.1007/978-3-319-12886-3_1
https://doi.org/10.1007/978-3-319-12886-3_1
Publikováno v:
Chinese Journal of Aeronautics. 19:134-150
Some years ago the national CFD project MEGAFLOW was initiated in Germany to combine many of the CFD development activities from DLR, universities and aircraft industry. Its goal was the development and validation of a dependable and efficient numeri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cea684e2871e51a4ac6c8d7148379ed6
https://doi.org/10.1016/s1000-9361(11)60293-8
https://doi.org/10.1016/s1000-9361(11)60293-8
This book reports on the German research initiative ComFliTe (Computational Flight Testing), the main goal of which was to enhance the capabilities of and tools for numerical simulation in flight physics to support future aircraft design and developm
Publikováno v:
52nd Aerospace Sciences Meeting.
The only implicit smoothing method implemented in the DLR Flow Solver TAU is the LU-SGS method. It was chosen several years ago because of its low memory requirements and low operation counts. Since in the past for many examples a severe restriction
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6961c04b96bce34ec50cacd1228129ad
https://doi.org/10.2514/6.2014-0080
https://doi.org/10.2514/6.2014-0080