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-averaged pressure spectra, typical power spectra are included for several representative conditions.
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April 1997
Research Papers
Measurement of Gust Response on a Turbine Cascade
A. P. Kurkov,
A. P. Kurkov
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135
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B. L. Lucci
B. L. Lucci
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135
Search for other works by this author on:
A. P. Kurkov
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135
B. L. Lucci
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135
J. Turbomach. Apr 1997, 119(2): 238-246 (9 pages)
Published Online: April 1, 1997
Article history
Received:
February 13, 1995
Online:
January 29, 2008
Citation
Kurkov, A. P., and Lucci, B. L. (April 1, 1997). "Measurement of Gust Response on a Turbine Cascade." ASME. J. Turbomach. April 1997; 119(2): 238–246. https://doi.org/10.1115/1.2841106
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