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基于实验的插板式进气畸变稳态压力场估计
引用本文:江勇,张发启,张百灵,孔卫东. 基于实验的插板式进气畸变稳态压力场估计[J]. 空军工程大学学报(自然科学版), 2007, 8(2): 1-3
作者姓名:江勇  张发启  张百灵  孔卫东
作者单位:空军工程大学,工程学院,陕西,西安,710038;空军工程大学,工程学院,陕西,西安,710038;空军工程大学,工程学院,陕西,西安,710038;空军工程大学,工程学院,陕西,西安,710038
摘    要:扰流插板引起的进气畸变流量随插板高度升高具有收敛到某一点的趋势。截面平均总压和周向低压区内平均总压与进气流量成线性关系。据此,可以预估周向畸变指数。低压区周向角只与插板高度成线性关系。截面稳态畸变压力分布可以分成高压区、掺混区、低压区,且分布各有特点,边界明显。

关 键 词:扰流插板  稳态进气畸变  压力分布  发动机
文章编号:1009-3516(2007)02-0001-03
收稿时间:2006-01-19
修稿时间:2006-01-19

The Inserted Board Air Inlet Flow Steady Pressure Distortion Field Estimate Based on Experiment
JIANG Yong,ZHANG Fa-qi,ZHANG Bai-ling,KONG Wei-dong. The Inserted Board Air Inlet Flow Steady Pressure Distortion Field Estimate Based on Experiment[J]. Journal of Air Force Engineering University(Natural Science Edition), 2007, 8(2): 1-3
Authors:JIANG Yong  ZHANG Fa-qi  ZHANG Bai-ling  KONG Wei-dong
Abstract:By an inserted board airflow inlet distortion test,the flow will be reduced to a point with raising the inserted board.The section average total pressure and the average total pressure in the circumferential low-pressure areas are in linear relationship with the air inlet flow.Then,the circumferential distortion exponent can be estimated.The circumferential angle in the low-pressure area just is in linear relationship to the inserted board height.The section steady distortion pressure distribution can be divided into high pressure area,mixing pressure area and low pressure area,each has its own characteristic in distortion and their boundaries are obvious.
Keywords:disturbed inserted board  steady air inlet flow distortion  pressure distribution  engine
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