Investigation of three-dimensional flow field in a turbine includingrotor/stator interaction. II - Three-dimensional flow field at the exit of the nozzle-Reference-Cited by-同舟云学术

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Investigation of three-dimensional flow field in a turbine includingrotor/stator interaction. II - Three-dimensional flow field at the exit of the nozzle

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

ZACCARIA M.¹,LAKSHMINARAYANA B.¹

Affiliation:

1. Pennsylvania State University, University Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3326

Reference29 articles.

1. Bammert,K., and Sandsteds, H.,1980,"Measurements ofthe Boundary Layer Development along B Turbine Blade with Rough Surfafsa," ASME Paper 80-GT-40.

2. Boleti., E. and Siaverding, C. H.,1984,"ExperimentalStudy of the Flow Field Behind an Annular Turbine Node Guide Vans with and without Downstream Rotor", ASME Paper 84-GT-16.

3. Ding, R.P., Joslyn, H.D. and Blair, M. F., 1987, "The Effeetsof Inlet Turbulenceand RotorfStator Interactionson the Aerodynamics and Heat Transfer of a Large-Scale Rotating TurbineModel", NASA-CR-179469, Vol. 4.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental and Numerical Investigation of Stator Exit Flow Field of an Automotive Torque Converter;Journal of Turbomachinery;1996-10-01

2. Time-Accurate Euler Simulation of Interaction of Nozzle Wake and Secondary Flow With Rotor Blade in an Axial Turbine Stage Using Nonreflecting Boundary Conditions;Journal of Turbomachinery;1996-10-01

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