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Keywords: NASA stage 37
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Proceedings Papers
Proc. ASME. GTINDIA2021, ASME 2021 Gas Turbine India Conference, V001T04A002, December 2–3, 2021
Paper No: GTINDIA2021-75881
... stage pressure ratio and efficiency decreases. transonic axial compressor vortex generator stall margin CFD NASA stage 37 Proceedings of the ASME 2021 Gas Turbine India Conference GTINDIA2021 December 2-3, 2021, Virtual, Online GTINDIA2021-75881 EFFECT OF AIRFOIL VORTEX GENERATOR...
Proceedings Papers
Proc. ASME. GTINDIA2021, ASME 2021 Gas Turbine India Conference, V001T04A003, December 2–3, 2021
Paper No: GTINDIA2021-75882
... treatment configurations. A maximum stall margin improvement of 3% was achieved with a particular slot configuration, but without any increase in compressor stage efficiency. transonic axial compressor slotted casing stall margin CFD NASA stage 37 Proceedings of the ASME 2021 Gas Turbine...
