Design and calibration of a certain aircraft/engine's simulation board

YE Wei; QIAO Wei-yang; HOU Min-jie

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Design and calibration of a certain aircraft/engine's simulation board

更新时间：2026-07-07

- Design and calibration of a certain aircraft/engine's simulation board
- Vol. 25, Issue 3, (2010)
- 作者机构：
  
  1. 西北工业大学动力与能源学院,西安,710072
  2. 中国航空工业集团公司中国燃气涡轮研究院,成都,610500
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2010
- 稿件说明：
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YE Wei, QIAO Wei-yang, HOU Min-jie. Design and calibration of a certain aircraft/engine's simulation board[J]. 2010, 25(3).
DOI：

YE Wei, QIAO Wei-yang, HOU Min-jie. Design and calibration of a certain aircraft/engine's simulation board[J]. 2010, 25(3). DOI：

摘要

为满足某型飞机/发动机相容性试验要求

提出了一种基于插板试验数据的半经验方法

用于模拟板的设计.在获得模拟板大致轮廓和阻力系数校验的基础上

通过模型的吹风校准试验和若干次环面基元畸变指数的调整

对比目标图谱的环面畸变强度和环面低压区大小

确定开孔的环面、孔的数量和孔的尺寸.结果表明

模拟的流场可满足某型飞机/发动机试验的要求.

Abstract

To satisfy the requirement of a certain aircraf/engine's compatibility test

this paper put forward a half-experience method based on the test data of flashboard for the design of simulation board.On the basis of obtained rough contour of the simulation board and the verifying of resistance coefficient

the given flow field's low pressure range and distortion intensity on the annular surface were compared by the model's blow test.For umpty adjustments of the distortion index of the annular surface element

it makes sure the annular surface holed

numbers and sizes of the holes.The results show that this method is simple and effective.The simulation flow field meets the needs of the certain aircraft/engine's test requirement.

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Related Author

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Related Institution

Science and Technology on Altitude Simulation Laboratory,Sichuan Gas Turbine Establishment,Aero Engine Corporation of China,Jiangyou Sichuan

School of Electronic Engineering,Xi’an Shiyou University

China Aviation Powerplant Research Institute, Aviation Industry Corporation of China

Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China, Shengyang

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