Gas Ingestion Under Unsteady Rotor-Stator Interaction of Turbine Blade
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-7652-0_5
Reference11 articles.
1. Phadke, U., Owen, J.: An investigation of ingress for an “air-cooled” shrouded rotating disk system with radial-clearance seals. J. Eng. Power 105, 178–183 (1983)
2. Phadke, U., Owen, J.: Aerodynamic aspects of the sealing of gas-turbine rotor-stator systems: Part 2: The performance of simple seals in a quasi-axisymmetric external flow. Int. J. Heat Fluid Flow 9(2), 106–112 (1988)
3. Bohn, D.E., Decker, A., Ohlendorf, N., Jakoby, R.: Influence of an axial and radial rim seal geometry on hot gas ingestion into the upstream cavity of a 1.5-stage turbine. ASME Paper No. GT2006-90453 (2006)
4. Patinios, M., Scobie, J.A., Sangan, C.M., et al.: Measurement and modeling of ingress in a new 1.5-stage turbine research facility. ASME J. Eng. Gas Turb. Power 139(1), paper No. 012603 (2017)
5. Green, T., Turner, A.B.: Ingestion into the upstream wheelspace of an axial turbine stage. J. Turbomach. 116(2), 327–332 (1994). https://doi.org/10.1115/1.2928368
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