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Autor:
Rütten, Markus, Zastrow, Jonas
Publikováno v:
AIAA AVIATION 2022 Forum.
Autor:
Rütten, Markus, Koch, Stefan
The Business Unit GUK of DNW proposed a research and development support in cooperation with the Institute of Aerodynamics and Flow Technology (DLR--AS) entitled "3D-Adaptation Procedure for the 2D-Adaptive Walls in the DNW-KRG Test Section''. The re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::3bcab39139d018e975b8027930ff1287
https://elib.dlr.de/137691/
https://elib.dlr.de/137691/
Autor:
Lindermeir, Erwin, Rütten, Markus
DLR´s capabilities in aircraft design are spread over many institutes which are located at various sites in Germany. With the Mephisto project DLR aims at combining this distributed expertise. The paper at hand reports on one aspect of this effort,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fd1d27d02dcb64528d21620d40b3da58
This paper presents results of current DLR research on the stability and control behavior of a generic flying wing configuration. The geometry considered here is a flying wing configuration with a leading edge sweep angle of 53°. The focus of the in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::df7c5e01936330e50aec83ce31dce724
Autor:
Rütten, Markus, Wünsch, Olaf
Non-Newtonian fluid properties can change the flow behaviour significantly, its prediction is more difficult when thermal effects come into play. Hence, the focal point of this work is the wake flow behind a heated circular cylinder in the laminar vo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3dd745ece4dc7e27be715b355b157f4e
https://elib.dlr.de/114376/
https://elib.dlr.de/114376/