The paper presents benchmark experimental data on a gust response of an annular turbine cascade. The experiment was particularly designed to provide data for comparison with the results of a typical linearized gust-response analysis. Reduced frequency, Mach number, and incidence were varied independently. Except for the lowest reduced frequency, the gust velocity distribution was nearly sinusoidal. For the high inlet-velocity series of tests, the cascade was near choking. The mean flow was documented by measuring blade surface pressures and the cascade exit flow. High-response pressure transducers were used to measure the unsteady pressure distribution. Inlet-velocity components and turbulence parameters were measured using hot wire. In addition to the synchronous time-average pressure spectra, typical power spectra are included for several representative conditions.
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ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition
June 5–8, 1995
Houston, Texas, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7882-8
PROCEEDINGS PAPER
Measurement of Gust Response on a Turbine Cascade
A. P. Kurkov,
A. P. Kurkov
National Aeronautics and Space Administration Lewis Research Center, Cleveland, OH
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B. L. Lucci
B. L. Lucci
National Aeronautics and Space Administration Lewis Research Center, Cleveland, OH
Search for other works by this author on:
A. P. Kurkov
National Aeronautics and Space Administration Lewis Research Center, Cleveland, OH
B. L. Lucci
National Aeronautics and Space Administration Lewis Research Center, Cleveland, OH
Paper No:
95-GT-096, V005T14A002; 10 pages
Published Online:
February 16, 2015
Citation
Kurkov, AP, & Lucci, BL. "Measurement of Gust Response on a Turbine Cascade." Proceedings of the ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award. Houston, Texas, USA. June 5–8, 1995. V005T14A002. ASME. https://doi.org/10.1115/95-GT-096
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