Effects of stationary wake on turbine blade heat transfer in a transonic cascade
The effects of a wake generated by a stationary upstream strut on surface heat transfer to turbine blades were measured experimentally. Time-resolved and unsteady heat flux measurements were made with Heat Flux Microsensors (HFM) at three positions on the suction surface and one position on the pres...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/44350 http://scholar.lib.vt.edu/theses/available/etd-08222008-063626/ |
| Summary: | The effects of a wake generated by a stationary upstream strut on surface heat
transfer to turbine blades were measured experimentally. Time-resolved and unsteady
heat flux measurements were made with Heat Flux Microsensors (HFM) at three
positions on the suction surface and one position on the pressure surface of a turbine
blade. The experiments were conducted on a stationary cascade of blades for heated runs
at transonic conditions
<p>Methods for determining the adiabatic wall temperature and heat transfer
coefficient are presented and the results are compared to computer predictions for these
blades. Heat transfer measurements were taken with new HFM-6 insert gages. A strong
influence on the heat transfer coefficient was seen from the relative position of the strut
with respect to the leading edge of the test blades. As the strut approached the leading
edge of the blade the heat transfer increased by 15% at gage location 2 on the suction
surface. The largest increase in .the heat transfer coefficient was seen on the pressure
surface. Results at this location show a 24% increase in the overall heat transfer
coefficient for one of the strut locations. The values obtained for the heat transfer
coefficients for the no strut case did not compare well with computer predictions. The
results did support the experimental results of other researchers, however. The fast time response of the HFM illustrated graphically an increase in the frequency energy between
the 0-10 kHz range when the strut was located near the leading edge of the instrumented
blade. The heat flux turbulence intensity (Tuq) was defined as another physical quantity
important to turbine blade heat transfer, but no conclusions could be drawn from the
results as to how this value compares to the turbulence intensity. === Master of Science |
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