Discussion: "The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade" [ASME J. Turbomach., 122, No. 3, pp. 416-424 (2000)]

被引：0

作者：

Cumpsty, NA ^{[1
]}

机构：

[1] Univ Cambridge, Dept Engn, Whittle Lab, Cambridge CB3 0DY, England

来源：

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 2000年 / 122卷 / 03期

关键词：

D O I：

10.1115/1.1287997

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：424 / 424

页数：1

共 8 条

[1] Closure to Discussion of ‘The Influence of Technical Surface Roughness Caused by Precision Forging on the Flow Around a Highly Loaded Compressor Cascade’ [ASME J. Turbomach., 122, No. 3, p. 424 (2000)]
Leipold, Robert
Boese, Matthias
Fottner, Leonhard
Journal of Turbomachinery, 2000, 122 (03):
[2] The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade
Leipold, R
Boese, M
Fottner, L
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 416 - 424
[3] Discussion: "Development of advanced compressor airfoils for heavy-duty gas turbines - Part II: Experimental and theoretical analysis" [ASME J. Turbomach., 122, No. 3, pp. 406-414 (2000)]
Cumpsty, NA
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 414 - 415
[4] Closure to "Discussion of 'Development of advanced compressor airfoils for heavy-duty gas turbines - Part II: Experimental and theoretical analysis' " [ASME J. Turbomach., 122, No. 3, pp. 406-414 (2000)]
不详
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 415 - 415
[5] Discussion: "On the development and application of the fast-response aerodynamic probe system in turbomachines - Part 3: Comparison of averaging methods applied to centrifugal compressor measurements" - [ASME J. Turbomach., 122, No. 3, pp. 527-535 (2000)]
Cumpsty, NA
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 536 - 536
[6] Closure to Discussion of ‘On the Development and Application of the Fast-Response Aerodynamic Probe System for Turbomachines—Part 3: Comparison of Averaging Methods Applied to Centrifugal Compressor Measurements’ [ASME J. Turbomach., 122, No. 3, p. 527–535 (2000)]
Kupferschmied, Peter
Journal of Turbomachinery, 2000, 122 (03):
[7] Discussion: "Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex" ( Mailach, R., Lehmann, I., and Vogeler, K., 2001, ASME J. Turbomach., 123, no. 3, pp. 453-460)
Cumpsty, NA
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2001, 123 (03): : 461 - 461
[8] Discussion: "An FFT-based transient flash temperature model for general three-dimensional rough surface contacts" ( Gao, J., Lee, S. C., Ai, X., and Nixon, H., 2000, ASME J. Tribol., 122, no. 3, pp. 519-523)
Abdel-Aal, HA
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 2000, 122 (04): : 876 - 876

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