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TECHNICAL PAPERS

An Investigation on Turbine Tip and Shroud Heat Transfer

[+] Author and Article Information
Kam S. Chana

QinetiQ, Cody Technology Park, Farnborough Hants, GU14 OLX UK

Terry V. Jones

Department of Engineering Science, University of Oxford, Oxford, OX1 3PJ UK

J. Turbomach 125(3), 513-520 (Aug 27, 2003) (8 pages) doi:10.1115/1.1575253 History: Received December 12, 2001; Online August 27, 2003
Copyright © 2003 by ASME
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References

Figures

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The ILPF turbine module
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Typical stage inlet total temperatures
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Measured radial temperature profiles
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Inlet temperature (K) for OTDF 1 and OTDF 2
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Rotor casing static pressure (Pa)
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Rotor casing static pressure time histories; blade surfaces and transducer positions indicated by vertical lines
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Rotor casing instantaneous static pressure fluctuations (Pa)
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Rotor casing instantaneous static pressure random unsteadiness
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Adiabatic wall temperature (K)
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Rotor casing Nusselt number based on rotor chord Nuc
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Typical transonic NGV shock structure
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Rotor casing Nusselt number Nuc for conditions given in Table 1
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Rotor casing heat transfer time histories
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Rotor casing instantaneous heat transfer rate fluctuations
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Rotor casing heat transfer rate random unsteadiness
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Rotor tip Nusselt number Nuc for conditions given in Table 1
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Rotor tip unsteady heat transfer rate
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Two-dimensional model of tip flow relative to the rotor

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