Vane-blade interaction in a transonic turbine. II - Heat transfer-Reference-Cited by-同舟云学术

Vane-blade interaction in a transonic turbine. II - Heat transfer

Published:1994-05 Issue:3 Volume:10 Page:312-317
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Rao K. V.¹,Delaney R. A.¹,Dunn M. G.²

Affiliation:

1. Allison Gas Turbine Division, Indianapolis, Indiana 46206

2. Calspan Advanced Technology Center, Buffalo, New York 14225

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.23758

Reference21 articles.

1. 'Hylton, L. D., Mihelc, M. S., Turner, E. R., Nealy, D. A., and York, R. E. "Analytical and Experimental Evaluation of Heat Transfer Distribution over Surfaces of Turbine Vanes,'7NASA CR 168015, May 1983.

2. Local Heat Transfer Measurements on a Gas Turbine Blade

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