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Keywords: transonic compressor
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Proceedings Papers
Proc. ASME. GT2022, Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V10AT29A040, June 13–17, 2022
Paper No: GT2022-83374
... compressor surge margin improvement casing treatment transonic compressor Proceedings of ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition GT2022 June 13-17, 2022, Rotterdam, The Netherlands GT2022-83374 TIP FLOW CONTROL IN OPTIMIZED LARGE GAS TURBINE COMPRESSOR BLADING Katja...
Proceedings Papers
Proc. ASME. GT2022, Volume 10C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions, V10CT32A031, June 13–17, 2022
Paper No: GT2022-82519
... period is limited. The method is demonstrated through the redesign of an axial transonic compressor (Darmstadt Transonic Compressor), which has been extensively studied by experimental research and numerical simulations. The interaction between the shock wave, the tip clearance flow, and the boundary...
Proceedings Papers
Proc. ASME. GT2022, Volume 2: Coal, Biomass, Hydrogen, and Alternative Fuels; Controls, Diagnostics, and Instrumentation; Steam Turbine, V002T05A017, June 13–17, 2022
Paper No: GT2022-82750
... the potential ability to operate capacitive probes at larger ranges and in poor SNR environments and gives a possible application in monitoring rotor blade integrity, at a low, additional computation time cost. blade tip clearance transonic compressor blade deflection turbomachinery digital filtering...
Proceedings Papers
Proc. ASME. GT2021, Volume 9A: Structures and Dynamics — Aerodynamics Excitation and Damping; Bearing and Seal Dynamics; Emerging Methods in Design and Engineering, V09AT23A014, June 7–11, 2021
Paper No: GT2021-59416
... Abstract The unsteady behavior of the shock wave was studied in an oscillating transonic compressor cascade. The experimental measurement and corresponding numerical simulation were conducted on the cascade with different shock patterns based on influence coefficient method. The unsteady...
Proceedings Papers
Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A030, June 7–11, 2021
Paper No: GT2021-59231
... airfoil, and then specialized for the optimization of a rotor in a 3-stage transonic compressor. The 3-stage transonic compressor studied in this paper is representative of the inlet stages of an industrial gas turbine, and the shock structure of the third rotor (R3) presents the peak strength near...
Proceedings Papers
Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A043, September 21–25, 2020
Paper No: GT2020-15064
... it is based is thus determined and its implications for blade design and manufacturing discussed. transonic compressor supersonic fan high-speed compressor transonic compressor relief TRANSONIC RELIEF IN FANS AND COMPRESSORS Demetrios Lefas, Robert J. Miller Whittle Laboratory University...
Proceedings Papers
Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T01A018, September 21–25, 2020
Paper No: GT2020-14571
... and direct calculation instead of proposing a judgment criterion. Three well-documented NASA axial transonic compressors are calculated by this meanline method, and the speedlines and aerodynamic parameters are compared with the experimental data to verify the method presented in this paper. A discussion...
Topics:
Compressors
Proceedings Papers
Proc. ASME. GT2019, Volume 7A: Structures and Dynamics, V07AT36A016, June 17–21, 2019
Paper No: GT2019-91468
.... transonic compressor flow induced vibration buffet stall flutter industrial gas turbine RIG TESTING OF THE OPERABILITY OF A TRANSONIC COMPRESSOR BLADE OF AN INDUSTRIAL GAS TURBINE Hyunsu Kang Doosan Heavy Industry Changwon, South Korea Sungjong Ahn Doosan Heavy Industry Changwon, South Korea Kyusic...
Proceedings Papers
Proc. ASME. GT2010, Volume 5: Industrial and Cogeneration; Microturbines and Small Turbomachinery; Oil and Gas Applications; Wind Turbine Technology, 135-156, June 14–18, 2010
Paper No: GT2010-23141
... for an isolated transonic compressor rotor (NASA rotor 37). The Model #1, representing spread phenomenon, assumes that all droplets impacting on the blade are trapped in the water film and subsequently released from its trailing edge and enter the wake region with an equivalent mass flow but bigger in diameter...