Numerical and experimental investigation of turbine tip gap flow
Author:
Affiliation:
1. Cambridge Univ., United Kingdom
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-2253
Reference14 articles.
1. [I] Bindon, J.P. "Pressure distributionsin the Tip Clearance Region of an Unshrouded Axial Turbine as Affecting the Problem of TipBurnout." ASMEPaper 87-GT-230.1987.
2. Booth, T.C. Dodge. P.R., and Hepworth, H.K. "Rotor-TipLeakagePartI-BasicMethodology,"ASMEPaper 81-GT71, 1981.
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