Effect of Inlet Spinner Shape on the Performance of a Low Aspect Ratio Transonic Axial Compressor Stage
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Non-IndexedPublished
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17th Annual CFD Symposium, NAL, BangaloreCite As
Maheshwaran, A., Subbaramu, S. and Nagpurwala, Q. H. (2015) Effect of Inlet Spinner Shape on the Performance of a Low Aspect Ratio Transonic Axial Compressor Stage, Proceedings of 17thAnnual CFD Symposium, NAL, Bangalore.
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