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[期刊论文] 作者：Piotr Doerffer,Oskar Szulc,,
来源：Journal of Thermal Science 年份：2007
Strong,normal shock wave,terminating a local supersonic area on an airfoil,not only limits aerodynamic per-formance but also becomes a source of a high-speed i...
[期刊论文] 作者：Piotr Doerffer,Oskar Szulc,Franco Magagnato,
来源：Journal of Thermal Science 年份：2003
The flow in transonic diffusers as well as in supersonic air intakes becomes often unsteady due to shock wave boundary layer interaction. The oscillations may...
[期刊论文] 作者：Piotr DOERFFER,Oskar SZULC,Rainer BOHNING,,
来源：Journal of Thermal Science 年份：2006
Normal shock wave, terminating a local supersonic area on an airfoil, limits its performance and becomes a source of high speed impulsive noise. It is proposed...
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