Statistical Analysis of Computational Fluid Dynamics Solutions from the Drag Prediction Workshop

2004 ◽  
Vol 41 (1) ◽  
pp. 95-103 ◽  
Author(s):  
Michael J. Hemsch
2003 ◽  
Vol 40 (5) ◽  
Author(s):  
David W. Levy ◽  
Tom Zickuhr ◽  
John Vassberg ◽  
Shreekant Agrawal ◽  
Richard A. Wahls ◽  
...  

2018 ◽  
Vol 55 (4) ◽  
pp. 1338-1351 ◽  
Author(s):  
Christopher J. Roy ◽  
Christopher L. Rumsey ◽  
Edward N. Tinoco

2005 ◽  
Vol 42 (5) ◽  
pp. 1165-1178 ◽  
Author(s):  
Kelly R. Laflin ◽  
Steven M. Klausmeyer ◽  
Thomas Zickuhr ◽  
John C. Vassberg ◽  
Richard A. Wahls ◽  
...  

Author(s):  
Baojie Liu ◽  
Jiaxin Liu ◽  
Xianjun Yu ◽  
Dejun Meng ◽  
Wenbin Shi

Abstract The results of previous studies have proved that manufacture variations can cause a noticeable influence on compressor aerodynamic performance. The main objective of this paper is to investigate the influence rules and mechanisms of manufacture variations on supersonic/transonic blades aerodynamic performance. The variations used in this study were measured from some newly manufactured high-pressure compressors. In the present study, several blade sections with different design Mach number conditions are selected for further statistical analysis of measured deviation data. Therefore, some systematic errors in the deviation data have been revealed. Based on these data, the computational fluid dynamics (CFD) method has been used to obtain the aerodynamic performances of a large number of the measured blade elements. And then, the analysis of the influence rules of manufacture variations on blade aerodynamic performance in different Mach number conditions has been carried out. The present results indicate that the effects of manufacture variations on blade aerodynamic performance in the lower Mach number (0.8) condition are much more significant comparing to that in the higher Mach number (0.9∼1.2) conditions. Based on this, influence mechanisms of manufacture variations on positive incidence range and negative incidence range have been analyzed. The differences of influence mechanisms in different Mach number conditions are the focus of research.


AIAA Journal ◽  
2003 ◽  
Vol 41 (9) ◽  
pp. 1647-1657 ◽  
Author(s):  
Luigi Paparone ◽  
Renato Tognaccini

2011 ◽  
Vol 2011 ◽  
pp. 1-8 ◽  
Author(s):  
Li Li ◽  
Bai Wen ◽  
Liang Yihua

In this paper some recent efforts for credible computational fluid dynamics (CFD) simulations in China are reviewed. The most important effort is that, following similar activities in the West such as ECARP and AIAA Drag Prediction Workshops, a series of workshops on credible CFD simulations had been initiated. These workshops were with ambitions to assess the status of CFD in China. Another major effort is an ongoing project to establish a software platform for studying the credibility of CFD solvers and performing credible CFD simulations. The platform, named WiseCFD, was designed to implement a seamless CFD process and to circumvent tedious repeating manual operations. It had also been a powerful job manager for CFD with capabilities to support plug and play (PnP) solver integration as well as distributed or parallel computations. Some future work on WiseCFD was proposed, and also envisioned was how WiseCFD and the European QNET-CFD Knowledge Base can benefit mutually.


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