Geometry effects on aerodynamics performance of a low aspect ratio turbine nozzle-Reference-Cited by-同舟云学术

Geometry effects on aerodynamics performance of a low aspect ratio turbine nozzle

Published:2004-11 Issue:4 Volume:13 Page:289-296
ISSN:1003-2169
Container-title:Journal of Thermal Science
language:en
Short-container-title:J. of Therm. Sci.

Author:

Chen Naixing,Zhang Hongwu,Xu Yanji,Huang Weiguang

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Link

http://link.springer.com/content/pdf/10.1007/s11630-004-0044-1.pdf

Reference18 articles.

1. Wang, Z Q, Lai, S K, Shu, W. Aerodynamic Calculation of Turbine Stator Cascade with Curvilinear Leaned Blades and Some Experimental Results. In: Proceedings of ISABE Conference, Bangalore, India, 1981

2. Wang, Z Q, et al. The Effect of Blade leaning on Cascade Aerodynamic Characteristics and the Experimental Study of Mechanism of Reduction Secondary Losses by Leaned Blade. Journal of Engineering Thermophysics, 1986, 9(2)

3. Breugelmans, F A E, Carels, Y, Demuth, M. Influence of Dihedral on the Secondary Flow in a Two-Dimensional Compressor Cascade. ASME Journal of Engineering for Gas Turbines and Power, 1984, 106: 577–584

4. Breugelmans, F A E. Investigation of Dihedral Effects in Compressor Cascades, AGARD CP421, Advanced Technology for Aero Gas Turbine Compressors, 1987

5. Sieverding, C H. Recent Progress in the Understanding of Basic Aspect of Secondary Flows in Turbine Blade Passage. ASME Journal of Engineering for Power, 1985, 107: 248–257

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