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从叶片表面静压分布分析弯曲扩压叶栅的能量损失
引用本文:吴继权,吴国钏,钟兢军,苏杰先,王仲奇.从叶片表面静压分布分析弯曲扩压叶栅的能量损失[J].航空动力学报,1998,13(2):118-122,216.
作者姓名:吴继权  吴国钏  钟兢军  苏杰先  王仲奇
作者单位:南京航空航天大学,哈尔滨工业大学
摘    要:对常规直叶片、正弯曲叶片及反弯曲叶片组成的3种平面扩压叶栅的叶片表面静压和出口流场在-5°,0°,5°及10°四个攻角下进行了测量,并给出了叶片表面静压分布特性及出口流场的能量损失分布特性。本文试图从叶片表面静压分布来分析弯曲扩压叶栅的能量损失机理,探讨不同弯曲叶片在扩压叶栅中应用的变工况性能。

关 键 词:弯曲  叶片  能量损失  静压力  分布
收稿时间:3/1/1997 12:00:00 AM
修稿时间:5/1/1997 12:00:00 AM

ANALYSIS OF ENERGY LOSSES FROM STATIC PRESSURE DISTRIBUTIONS ON BLADE SURFACES IN CURVED CASCADES
Wu Jiquan,Wu Guochuan,Zhong Jingjun,Su Jiexian and Wang Zhongqi.ANALYSIS OF ENERGY LOSSES FROM STATIC PRESSURE DISTRIBUTIONS ON BLADE SURFACES IN CURVED CASCADES[J].Journal of Aerospace Power,1998,13(2):118-122,216.
Authors:Wu Jiquan  Wu Guochuan  Zhong Jingjun  Su Jiexian and Wang Zhongqi
Institution:2nd Dept.Nanjing University of Aeronautics and Astronautics,Nanjing 210016;2nd Dept.Nanjing University of Aeronautics and Astronautics,Nanjing 210016;Energy Science and Engineering College,Harbin Institute of Technology,Harbin 150001;Energy Science and Engineering College,Harbin Institute of Technology,Harbin 150001;Energy Science and Engineering College,Harbin Institute of Technology,Harbin 150001
Abstract:The exit flow field and the static pressure on the blade surface for three sets of different cascades were measured at four incidences of -5°,0°,5° and 10° respectively in a low-speed cascade wind tunnel.The three sets were a conventional straight cascade,a positive curved one and a negative curved one.The static pressure distributions on blade surfaces and the energy loss distribution in the exit flow fields have been obtained.The purpose of this paper is to find out the energy loss mechanism of the curved blade cascades from the static pressure distribution on the blade surface,and to study performance of compressor cascades at different incidences.
Keywords:Bending  Cascades  Static pressure  Distribution
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