Numerical insight into flow and thermal patterns within an inlet profile generator comparing to experimental results

V. R. Kunze, M. Wolff, Michael David Barringer, Karen Ann Thole, M. D. Polanka

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    4 Citations (Scopus)

    Abstract

    Historically the design of gas turbine engines have not considered the interaction between the combustor and turbine stages. High pressure turbine varie stages have been designed assuming inlet conditions consistent with a standard turbulent boundary layer profile. However, combustor exit flow entering the vane is known to be highly non-uniform in both the primary and secondary flow regimes. In order to develop higher performance, more efficient, longer life stages, turbine design must take into account combustor exit non-uniformities. The Turbine Research Facility (TRF) at Wright-Patterson Air Force Base has installed a non-reactive full scale annular combustor simulator or more accurately a turbine inlet profile generator to study combustor-vane interaction. Several benchmark tests have been performed on the profile generator consisting of a Taguchi type matrix wherein nine independent variables were adjusted. Supplementing the experimental research at the TRF, a steady state, unstructured, fully three-dimensional CFD analysis was performed. This paper will make comparisons between the CFD and experimental profiles generated by the simulator. Furthermore, the computational study will help to give an understanding of the aerodynamic and aerothermal environment within the generator that experimental instrumentation alone cannot.

    Original languageEnglish (US)
    Title of host publicationProceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air
    Pages271-283
    Number of pages13
    Volume3 PART A
    DOIs
    StatePublished - Nov 15 2006
    Event2006 ASME 51st Turbo Expo - Barcelona, Spain
    Duration: May 6 2006May 11 2006

    Other

    Other2006 ASME 51st Turbo Expo
    CountrySpain
    CityBarcelona
    Period5/6/065/11/06

    Fingerprint

    Turbines
    Combustors
    Computational fluid dynamics
    Simulators
    Secondary flow
    Hot Temperature
    Gas turbines
    Aerodynamics
    Boundary layers
    Air

    All Science Journal Classification (ASJC) codes

    • Engineering(all)

    Cite this

    Kunze, V. R., Wolff, M., Barringer, M. D., Thole, K. A., & Polanka, M. D. (2006). Numerical insight into flow and thermal patterns within an inlet profile generator comparing to experimental results. In Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air (Vol. 3 PART A, pp. 271-283) https://doi.org/10.1115/GT2006-90276
    Kunze, V. R. ; Wolff, M. ; Barringer, Michael David ; Thole, Karen Ann ; Polanka, M. D. / Numerical insight into flow and thermal patterns within an inlet profile generator comparing to experimental results. Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. Vol. 3 PART A 2006. pp. 271-283
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    Kunze, VR, Wolff, M, Barringer, MD, Thole, KA & Polanka, MD 2006, Numerical insight into flow and thermal patterns within an inlet profile generator comparing to experimental results. in Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. vol. 3 PART A, pp. 271-283, 2006 ASME 51st Turbo Expo, Barcelona, Spain, 5/6/06. https://doi.org/10.1115/GT2006-90276

    Numerical insight into flow and thermal patterns within an inlet profile generator comparing to experimental results. / Kunze, V. R.; Wolff, M.; Barringer, Michael David; Thole, Karen Ann; Polanka, M. D.

    Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. Vol. 3 PART A 2006. p. 271-283.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

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    Kunze VR, Wolff M, Barringer MD, Thole KA, Polanka MD. Numerical insight into flow and thermal patterns within an inlet profile generator comparing to experimental results. In Proceedings of the ASME Turbo Expo 2006 - Power for Land, Sea, and Air. Vol. 3 PART A. 2006. p. 271-283 https://doi.org/10.1115/GT2006-90276