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Akademický článek
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In this paper two approaches are investigated to reduce the parasite drag of a helicopter. The first approach is to optimize the surface of the fuselage back door. This is done by applying an automatic, adjoint-based optimization chain; developed by
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::f3f9329837a77d4b71a46b42ae859798
https://elib.dlr.de/92943/
https://elib.dlr.de/92943/
Autor:
Resch, Michael, Bönisch, Thomas, Benkert, Katharina, Bez, Wolfgang, Furui, Toshiyuki, Seo, Yoshiki, Zhang, Qinyin, Bui, Phong, El-Askary, Wageeh A., Meinke, Matthias, Schröder, Wolfgang
Publikováno v:
High Performance Computing on Vector Systems; 2006, p139-153, 15p
Autor:
Hirschel, Ernst Heinrich, Fujii, Kozo, Haase, Werner, Leer, Bram, Leschziner, Michael A., Pandolfi, Maurizio, Periaux, Jacques, Rizzi, Arthur, Roux, Bernard, Shokin, Yurii I., Kroll, Norbert, Fassbender, Jens K., Zhang, Qinyin, Meinke, Matthias, Schröder, Wolfgang
Publikováno v:
MEGAFLOW - Numerical Flow Simulation for Aircraft Design; 2005, p241-250, 10p
Publikováno v:
Aerospace; Volume 10; Issue 3; Pages: 276
The need for environmentally responsible solutions in aircraft technology is now considered the priority for global challenges related to the limited supply of traditional fuel sources and the potential global hazards associated with emissions produc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9d253f34ce5b9a83f2d78b610cad710b
https://doi.org/10.3390/aerospace10030276
https://doi.org/10.3390/aerospace10030276