Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

TIAN Xiao-pei; SHAN Peng

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

基金项目: Programme of Introducing Talents of Discipline to Universities(B08009)

计量
- 文章访问数: 2834
- HTML浏览量: 4
- PDF量: 983
- 被引次数: 0
出版历程
- 收稿日期: 2012-10-07
- 刊出日期: 2013-07-28

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Funds: Programme of Introducing Talents of Discipline to Universities(B08009)

摘要

摘要: Two strategies extended the single-cascade methods from a compressible three-dimensional inverse method for radial and mixed flow turbomachines to two three-dimensional multi-cascade co-design methods for single-stage centrifugal compressors.These two three-dimensional methods and a typical quasi-three-dimensional streamline curvature through-flow inverse method were employed to design the same subsonic high-speed single-stage centrifugal compressors.The compressor performances were simulated by a commercial Reynolds averaged Navier-Stokes (RANS) equations solver.The studies show that two three-dimensional co-design methods are reasonable and feasible.It was found that:firstly the blade camber angle designed by the three-dimensional methods was larger than that designed by the quasi-three-dimensional method;and secondly with regard to two three-dimensional methods with different boundary conditions,the co-design result differences between the diffusers were small,but those between the deswirlers were relatively large.
- centrifugal compressor /
- through-flow inverse method /
- three-dimensional inverse problem
Abstract: Two strategies extended the single-cascade methods from a compressible three-dimensional inverse method for radial and mixed flow turbomachines to two three-dimensional multi-cascade co-design methods for single-stage centrifugal compressors.These two three-dimensional methods and a typical quasi-three-dimensional streamline curvature through-flow inverse method were employed to design the same subsonic high-speed single-stage centrifugal compressors.The compressor performances were simulated by a commercial Reynolds averaged Navier-Stokes (RANS) equations solver.The studies show that two three-dimensional co-design methods are reasonable and feasible.It was found that:firstly the blade camber angle designed by the three-dimensional methods was larger than that designed by the quasi-three-dimensional method;and secondly with regard to two three-dimensional methods with different boundary conditions,the co-design result differences between the diffusers were small,but those between the deswirlers were relatively large.
- centrifugal compressor /
- through-flow inverse method /
- three-dimensional inverse problem

HTML

参考文献(21)

[1]	Wu C.A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-,radial-,and mixed-flow types [R].NACA Technical Note 2604,1952.
[2]	Demeulenaere A,Van den Braembussche R.Three-dimensional inverse method for turbomachinery blading design[J].ASME Journal of Turbomachinery,1998,120(4):247-255.
[3]	Dang T.A fully three-dimensional inverse method for turbomachinery blading in transonic flows[J].ASME Journal of Turbomachinery,1993,115(4):354-361.
[4]	Tan C S,Hawthorne W R,Wang C,et al.Theory of blade design for large defections:Part Ⅱ annular cascades[J].ASME Journal of Engineering for Gas Turbines and Power,1984,106(2):354-365.
[5]	Dang T,Damle S,Qiu X.Euler-based inverse method for turbomachine blades:Part Ⅱ three dimensions flows[J].AIAA Journal,2000,38(11):2007-2013.
[6]	Ji M,Dang T,Cave M J.Fully three-dimensional viscous semi-inverse method for subsonic mixed-flow and radial impeller design[R].ASME Paper GT-2009-59679,2009.
[7]	Borges J E.A three-dimensional inverse method for turbomachinery:Part Ⅰ theory[J].ASME Journal of Turbomachinery,1990,112(3):346-354.
[8]	Zangeneh M,Hawthorne W R.A fully compressible three-dimensional inverse design method applicable to radial and mixed flow turbomachines [R]. ASME Paper 90-GT-198, 1990.
[9]	Zangeneh M.Inviscid-viscous interaction method for three-dimensional inverse design of centrifugal impellers[J]. ASME Journal of Turbomachinery,1994,116(2):280-290.
[10]	Damle S V,Dang T,Stringham J,et al.Practical use of three-dimensional inverse method for compressor blade design[J].ASME Journal of Turbomachinery,1999,121(4):321-325.
[11]	Demeulenaere A,Leonard O,Van den Braembussche R V D.Application of a three-dimensional inverse method to the design of a centrifugal compressor impeller [R].ASME Paper 98-GT-127,1998.
[12]	Veress A,Van den Braembussche R V D.Inverse design and optimization of a return channel for a multistage centrifugal compressor[J].ASME Journal of Fluids Engineering,2004,126(9):799-806.
[13]	Yang Y L,Tan C S,Hawthorne W R.Aerodynamic design of turbomachinery blading in three-dimensional flow:an application to radial inflow turbines[J].ASME Journal of Turbomachinery,1993,115(7):602-613.
[14]	Zangeneh M,Roduner D V C.Improving a vaned diffuser for a given centrifugal impeller [R].ASME Paper GT-2002-30621,2002.
[15]	Zangeneh M,Schleer M,Ploger F,et al.Investigation of an inversely designed centrifugal compressor stage:Part Ⅰ design and numerical verification[J].ASME Journal of Turbomachinery,2004,126(1):73-81.
[16]	Bonaiuti D,Zangeneh M,Aartojarvi R,et al.Parametric design of a waterjet pump by means of inverse design,CFD calculations and experimental analyses[J].ASME Journal of Fluids Engineering,2010,132(3):031104.1-031104.15.
[17]	Van Rooij M P C,Dang T Q,Larosiliere L M.Improving aerodynamic matching of axial compressor blading using a three-dimensional multistage inverse design method[J]. ASME Journal of Turbomachinery,2007,129(1):108-118.
[18]	Tian X,Shan P.A compressible three-dimensional inverse design method based on the streamline curvature approach and Clebsch formulation for radial and mixed flow turbomachines [R].ASME Paper POWER2012-54805,2012.
[19]	TIAN Xiaopei,SHAN Peng.Numerical investigation of the boundary conditions and Fourier series truncation errors for a 3-D inverse method for radial- and mixed-flow turbomachines[J].Journal of Aerospace Power.2013,28(2):390-400.(in Chinese)
[20]	TIAN Xiaopei,SHAN Peng.Improvements of Qiu slip factor model applied for quasi-3-D through-flow design of small centrifugal impellers[J].Journal of Aerospace Power,2010,25(11):2539-2547.(in Chinese)
[21]	NUMECA International.FINETM user manual version 6.2-b [R].Brussels,Belgium:FINETM Company,2004.

施引文献

资源附件(0)

访问统计

点击查看大图

计量

文章访问数: 2834
HTML浏览量: 4
PDF量: 983
被引次数: 0

姓名
邮箱
手机号码
标题
留言内容
验证码

留言板

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

计量

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

计量

目录

留言板

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

计量

出版历程

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

计量

出版历程

目录