期刊文献+

关于叶轮机时均(准四维)和非定常(四维)气动设计体系的初步诠释 被引量:7

ELEMENTARY ANNOTATION ABOUT TIME-AVERAGE (Q4D) AND UNSTEADY (4D) AERO-DYNAMIC DESIGN SYSTEM FOR TURBOMACHINERY
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摘要 本文以考虑非定常流动的完整性为线索,总结概述了先前气动设计体系的困难与限制,在此基础上,以描述叶轮机流动的时均和时间精确模型为核心分别从其构成和标志性技术对叶轮机时均和非定常气动设计体系进行了初步诠释。文章认为促成时均(准四维)和非定常(四维)气动设计体系现实应用是叶轮机发展的最后契机。 According to the integrality of considering about flow unsteadiness, the difficulties and limitations of the previous aerodynamic design systems are summarized. On the basis of Time-Average and Time-Accurate flow models, the constitution and key techniques of the time-average and unsteady aerodynamic design system are described. It is remarked that the advancement towards the time-average and unsteady aerodynamic design will be the eventual opportunities to promote the turbomachinery technology.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2003年第4期570-574,共5页 Journal of Engineering Thermophysics
基金 中国科学院知识创新工程项目(No.KGCX2-30) 国家自然科学基金(No.59906012) 国家重点基础研究发展规划项目(No.G1999022305)
关键词 非定常设计 叶轮机 缘线匹配 时均流动 unsteady design turbomachinery edge-matching time-average flow
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参考文献8

  • 1季路成,项林,徐建中,陈江.非定常环境下叶栅性能的数值研究[J].工程热物理学报,2003,24(2):211-215. 被引量:9
  • 2季路成 陈江 黄海波等.叶轮机时均(准四维)和非定常(四维)气动设计体系的初步诠释[A]..工程热物理学会热机气动热力学学术会议论文集[C].中山,2002.348—369.
  • 3He L, Chen T, et al. Analysis of Rotor-Rotor and Stator-Stator Interferences in Multi-Stage Turbomachines. ASME GT-2002-30355, 2002.
  • 4Curtis E M, Hodson H P. et al. Development of Blade Profiles for Low Pressure Turbine Applications. ASME J. of Turbomachinery, 1997, 119.
  • 5Adamczyk J J, Model Equation for Simulating Flows in Multistage Turbomachinery. NASA TM-86869, 1984.
  • 6Giles M. An Approach for Multi-Stage Calculations Incorporating Unsteadiness. ASME 92-GT-282, 1992.
  • 7Denton J D. The Calculation of Three Dimensional Viscous Flow Through Multistage Turbomachines. ASME90-GT-19, 1990.
  • 8Rhie C M, et al. Development and Application of a Multistage Navier-Stokes Solver, Part 1: Multistage Modeling Using Body-Forces and Deterministic Stresses. ASME95-GT-342, 1995.

二级参考文献5

  • 1[1]Huber F W, Johnson P D, Sharma O P, et al. Performance Improvement Through Indexing of Turbine Airfoils: Part I-Experimental Investigation. ASME 95-GT-27, 1995
  • 2[2]Halstead D E, Wisler D C, Okiishi T H, et al. Boundary Layer Development in Axial Compressors and Turbines,Part 1of 4:Composite Picture. ASME 95-GT-461, 1995
  • 3[3]Liu J S, Sockol P M. Unsteady Euler Cascade Analysis.AIAA 89-0322, 1989
  • 4[4]Giles M. An Approach for Multi-Stage Calculations Incorporating Unsteadiness. ASME 92-GT-282, 1992
  • 5[5]He L, Chen T, et al. Analysis of Rotor-Rotor and Stator-Stator Interferences in Multi-Stage Turboma-chines .ASME GT-2002-30355,2002

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