Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Juliane Nies"'
Publikováno v:
Aerospace Science and Technology. 81:65-77
In transonic airfoil flow, pressure waves are generated mainly at the trailing edge and in the case of a shock in the region of the shock/boundary layer interaction. Depending on the Mach number, these waves lead to oscillating shock waves and an uns
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b92e50cca970abab846b04ba62cc9d6
https://doi.org/10.1016/j.ast.2018.05.011
https://doi.org/10.1016/j.ast.2018.05.011
Publikováno v:
SAE Technical Paper Series.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78aab0117e8223040f02c2be9efc170d
https://doi.org/10.4271/2019-01-0646
https://doi.org/10.4271/2019-01-0646
Publikováno v:
Experiments in Fluids. 56
An investigation of pressure waves in compressible subsonic and transonic flow around a generic airfoil is performed in a modified shock tube. New comprehensive results are presented on pressure waves in compressible flow. For the first time, the inf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a349b9666ea57ccc41cc820c7bc45cc3
https://doi.org/10.1007/s00348-015-2009-4
https://doi.org/10.1007/s00348-015-2009-4
Autor:
Juliane Nies, Herbert Olivier
Publikováno v:
32nd AIAA Applied Aerodynamics Conference.
Trailing-edge brushes on a supercritical airfoil are investigated in order to analyze their influence on upstream-moving pressure waves evolving from the trailing edge. The upstream-moving pressure waves show a highly-instationary behavior which sign
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b574191528e46cf1a1e97c8254e9aaff
https://doi.org/10.2514/6.2014-3244
https://doi.org/10.2514/6.2014-3244
Publikováno v:
28th International Symposium on Shock Waves ISBN: 9783642256844
Upstream moving pressure waves are observed in transonic flows over airfoils already for decades. They can be generated actively by flap or airfoil oscillations [6]. But, they are also naturally present in airfoil flows [1, 4]. Upstream moving pressu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45a527fa409e34e3ce27d903202c52e2
https://doi.org/10.1007/978-3-642-25685-1_76
https://doi.org/10.1007/978-3-642-25685-1_76
