Open AccessDiscussion: “Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field” (Schulz, H. D., Gallus, H. E., and Lakshminarayana, B., 1990, ASME J. Turbomach., 112, pp. 679–688)
Author(s) -
N. A. Cumpsty,
Yanyang Dong
Publication year - 1990
Publication title -
journal of turbomachinery
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.972
H-Index - 112
eISSN - 1528-8900
pISSN - 0889-504X
DOI - 10.1115/1.2927709
Subject(s) - stator , cascade , rotor (electric) , gas compressor , flow (mathematics) , field (mathematics) , mechanics , physics , axial compressor , unsteady flow , aerospace engineering , engineering , mechanical engineering , mathematics , chemical engineering , pure mathematics
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