Noise Analysis of Turbo Prop Aircraft(C90GT)

터보프롭 항공기(C90GT)의 소음 분석

  • Ryu, Jong-Hyeon (Dept. of Flight Operation, Chodang University) ;
  • Kim, Woo-Jin (Dept. of Aviation Maintenance, Catholic Kwandong University) ;
  • Kim, Gyou-Beom (Dept. of Unmanned Aviation System Engineering, Catholic Kwandong University)
  • 류종현 (초당대학교 항공운항학과) ;
  • 김우진 (가톨릭관동대학교 항공정비학과) ;
  • 김규범 (가톨릭관동대학교 무인항공학과)
  • Received : 2019.07.16
  • Accepted : 2019.09.20
  • Published : 2019.09.27


The aircraft noise analysis area in this study is a training airfield where various kinds of aircraft are operated. It is difficult to identify the noise analysis as a real measurement in a training airfield. In order to overcome these practical limitations and to establish appropriate noise countermeasures, a noise map is prepared using the Integrated Noise Model Version 7.0 of the aircraft noise prediction program used by the FAA. The noise of C90GT aircraft was measured while flying the takeoff route, landing route, and long route. We want to identify areas where noise damage is more than 70 WECPNL. No area exceeding the legal standard of 70 WECPNL was found in all routes.


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