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• W2034508964 abstract "This note reviews the widely used phased-lagged [Erdos, J. L., E. Alzner, and W. McNally. 1977 Erdos, J. I., Alzner, E. and McNally, W. 1977. Numerical Solution of Periodic Transonic Flow Through a Fan Stage. AIAA Journal, 15(11): 1559–68. doi:10.2514/3.60823[Crossref], [Web of Science ®] , [Google Scholar]. AIAA Journal 15: 1559–68.] approach and corresponding chorochronic interface relations [Gerolymos G. A., G. J. Michon, and J. Neubauer. 2002. Journal of Propulsion and Power 18: 1139–52.] and explores its potential extension to the approximate unsteady throughflow analysis of multistage turbomachinery. The basic relations pertaining to the binary blade-row interaction case, for which chorochronic periodicity is exact in a phase-averaged rans framework, are briefly formulated, and selected computational examples illustrate the application of the method. Then, the filtered chorochronic interface is defined as the unsteady counterpart of the well-known mixing-plane concept. This interface takes into account only those tθ-waves which are compatible with the interaction of the immediately upstream and downstream blade-rows. The concept, which is similar to the decomposition-and-superposition method [Li, H. D., and L. He. 2005 Li, H. D. and He, L. 2005. Toward Intra-row Gap Optimization of -stage Transonic Compressor. ASME Journal of Turbomachinery, 127: 589–98. doi:10.1115/1.1928934[Crossref], [Web of Science ®] , [Google Scholar]. ASME J ournal of Turbomachinery 127: 589–98.], is illustrated by 3-D computations of a ½-stage transonic compressor." @default.
• W2034508964 created "2016-06-24" @default.
• W2034508964 creator A5056222323 @default.
• W2034508964 date "2013-02-01" @default.
• W2034508964 modified "2023-09-25" @default.
• W2034508964 title "Filtered chorochronic interface as a capability for 3-D unsteady throughflow analysis of multistage turbomachinery" @default.
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• W2034508964 doi "https://doi.org/10.1080/10618562.2013.772984" @default.
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