The interaction between consecutive blade rows can be expected to have important effects on the heat transfer in cooled gas turbine cascades. In determining the local heat transfer under the influence of wake flow, nonintrusive optical measuring techniques were used to obtain the flow velocities and turbulence structures in the cascade inlet flow as well as along the test blade’s surface. The main purpose of the measurements is to provide accurate experimental data for the development of predictive codes. The applicability primarily of the laser-Doppler technique is discussed and problems arising from the use of laser-dual-focus anemometry are reported. In simulating the effects of wake flow, a plane airfoil was traversed in front of the cascade. Both the axial distance between the airfoil and the cascade and the position in circumferential direction were changed in discrete steps. Turbulence intensities between 1.4 and 15 percent were recorded in cold gas flow. The effects on the blade heat transfer are illustrated.
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April 1987
Research Papers
Laser-Doppler Studies of the Wake-Effected Flow Field in a Turbine Cascade
S. Wittig,
S. Wittig
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
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K. Dullenkopf,
K. Dullenkopf
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
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A. Schulz,
A. Schulz
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
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R. Hestermann
R. Hestermann
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
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S. Wittig
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
K. Dullenkopf
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
A. Schulz
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
R. Hestermann
Lehrstuhl und Institut fu¨r Thermische Stro¨mungsmaschinen, Universita¨t Karlsruhe (T.H.), D-7500 Karlsruhe 1, Federal Republic of Germany
J. Turbomach. Apr 1987, 109(2): 170-176 (7 pages)
Published Online: April 1, 1987
Article history
Received:
February 7, 1986
Online:
November 9, 2009
Citation
Wittig, S., Dullenkopf, K., Schulz, A., and Hestermann, R. (April 1, 1987). "Laser-Doppler Studies of the Wake-Effected Flow Field in a Turbine Cascade." ASME. J. Turbomach. April 1987; 109(2): 170–176. https://doi.org/10.1115/1.3262082
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