Volume 13, Issue 12 (2-2014)
Modares Mechanical Engineering 2014, 13(12): 1-13 |
Back to browse issues page
Download citation:
BibTeX | RIS | EndNote | Medlars | ProCite | Reference Manager | RefWorks
Send citation to:
BibTeX | RIS | EndNote | Medlars | ProCite | Reference Manager | RefWorks
Send citation to:
Azizi R. The Novel Preliminary Design Algorithm of Multistage Axial Compressors through Two Layer Multi-Objective/Multi-Variables Optimization. Modares Mechanical Engineering 2014; 13 (12) :1-13
URL: http://mme.modares.ac.ir/article-15-4373-en.html
URL: http://mme.modares.ac.ir/article-15-4373-en.html
1- PHD Candidate
Abstract: (6051 Views)
The preliminary design of multistage axial compressor requires a vast number of design variables and limitations, the simultaneous investigation of which needs a complicated design program. This study provides a new algorithm by the use of combining multi-variable/multi-objective optimizations, meanline simulator and preliminary design program. On the one hand the two-layer optimization is used to consider all design variables and on the other the design limitations are put into the cost function together with surge margin and efficiency. The comparison of the results with the NASA transonic eight-stage compressor shows the ability of the new algorithm to achieve a compressor with better performance and lower weight.
Keywords: Preliminary design, Multi Variable/Multi Variable Optimization, Meanline Simulator, Velocity Triangles
Article Type: Research Article |
Subject:
Aerodynamics|Thermodynamics|Gas Dynamics
Received: 2013/05/26 | Accepted: 2013/07/2 | Published: 2013/12/21
Received: 2013/05/26 | Accepted: 2013/07/2 | Published: 2013/12/21
| Rights and permissions | |
 |
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License. |