Abstract
Unsteady surface pressure and heat transfer have been measured on a blade of a linear turbine cascade exposed to unsteady oncoming wakes generated by moving cylinders on a squirrel cage device. The Reynolds number and the Strouhal number corresponded to the values in a real turbomachine. The periodic components of pressure and heat transfer showed clear response to the unsteady wakes. However, the distribution along the blade surface of both pressure and heat transfer coefficient changed very little from phase to phase. The heat transfer results have shown that the boundary layer on the pressure side remained laminar for all cases, but that the boundary layers on the suction side became transitional under the wake disturbance. With increasing wake-passing frequency, the start of the transition moved forward. Increasing the wake-passing frequency resulted in a significant increase in heat transfer along the whole blade surface including the portions where the boundary layers were nominally laminar.
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Abbreviations
- C p :
-
pressure coefficient
- dt :
-
time step of data acquisition
- F :
-
any measured instantaneous quantity
- 〈F〉:
-
ensemble average
- F′:
-
turbulent fluctuation
- \(\bar F\) :
-
time average
- \(\tilde F\) :
-
periodic component
- f :
-
cylinder-passing frequency
- h :
-
heat transfer coefficient
- p :
-
pressure
- q c :
-
convective heat transfer rate per unit area
- s :
-
blade surface arc length coordinate
- s o :
-
blade surface arc length from leading edge to trailing edge
- Str:
-
Strouhal number = f × chord/U inf
- T :
-
cylinder-passing period
- T e :
-
free stream flow temperature
- Tu :
-
turbulence level
- T w :
-
blade surface temperature
- U :
-
velocity component in x-direction for blade to blade flow, or streamwise velocity component in boundary layer
- V :
-
velocity component in y-direction
- x :
-
x-coordinate
- y :
-
y-coordinate
- ϱ :
-
air density
- v :
-
kinematic viscosity of air
- cyl:
-
cylinder
- e :
-
external
- inf:
-
oncoming flow condition
References
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The work reported here was sponsored by the German Federal Ministry of Research and Technology through program TURBOTHERM under contract no. 0326501D. The authors should like to thank Mr. D. Bierwirth for his excellent technician work on this project, Dr. N. H. Cho for his help with the preparation of the plots and Mrs. R. Zschernitz for her expert typing of the text.
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Liu, X., Rodi, W. Surface pressure and heat transfer measurements in a turbine cascade with unsteady oncoming wakes. Experiments in Fluids 17, 171–178 (1994). https://doi.org/10.1007/BF00190914
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DOI: https://doi.org/10.1007/BF00190914