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飞机进气道/发动机匹配工作流场测试和分析 被引量:3

Test and Analysis of the Flow Field on Air Inlet/Engine Matching Operation
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摘要 在介绍全尺寸飞机进气道/发动机匹配工作流场测试系统的基础上,给出了在发动机前安装飞机前机身后,在地面台架试车时测得的进口压力场数据,计算了进口压力场的畸变指数,分析了流场畸变图谱。 Based on introducing the flow field test system on air inlet/engine matching opration with whole size, when the forebody is installed ahead of the engine, the inlet pressure field data measured on the ground test platform are given. The distortion index has been calculated and the distortion map of the pressure field has been analyzed.
出处 《航空计测技术》 1998年第5期11-13,共3页 Aviation Metrology & Measurement Technology
关键词 匹配工作 流场测试 飞机 进气道 发动机 Matching operation ,Flow field test, Distortion index,Distortion map
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  • 1李大伟,张云飞,马东立.背负式S形进气道设计及数值分析[J].推进技术,2006,27(1):61-65. 被引量:12
  • 2Tormalm M. Design and analysis of compact UAV ducts [ R ]. AIAA 2006-2828,2006.
  • 3Kirk A M, Gargoloff J I, Rediniotis OK, et. al. Numerical and experimental investigation of a serpentine inlet duct [ R ]. AIAA 2007 -842,2007.
  • 4Beale D K,Zelenakt M. Development and validation of a freejet technique for inlet-engine compatibility testing [ R ]. AIAA-92- 3921,1992.
  • 5Lee K, Lee B, Kang S,et al. Inlet distortion test with gas turbine engine in the altitude engine test facility[ R 1. AIAA-2010-4337, 2010.
  • 6Sutlif D L, Konno K E, HeiDelberg L J. Duct mode measurements on the TFE731-60 full scale engine[ R]. AIAA-2002-2564.
  • 7Weir D, Bouldin B, Mendoza J. Static and flight aeroacoustic evaluations of a scarf inlet [ R ]. AIAA-2006-2462,2006.
  • 8Danielle K L, Validation of the predicted circumferential and radial mode sound power levels in the inlet and exhaust ducts of a fan ingesting distorted inflow [ R ]. AIAA-2011-2808,2011.
  • 9叶巍,乔渭阳,侯敏杰.某型飞机/发动机模拟板设计与校准[J].航空动力学报,2010,25(3):641-646. 被引量:8
  • 10汪涛,姜健,史建邦.进气道/发动机相容性试飞中总压畸变数据的采集与处理[J].燃气涡轮试验与研究,2012,25(2):54-58. 被引量:9

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