Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
2017 / 01
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Adaptive mesh refinement method based investigation of the interaction between shock wave, boundary layer, and tip vortex in a transonic compressor
Gou, Jinlan, Yuan, Xin, Su, XinrongLanguage:
english
Journal:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
DOI:
10.1177/0954410016687142
Date:
January, 2017
File:
PDF, 2.51 MB
english, 2017