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A Research of the Flow-Field Measurement Above the Flight Deck on LHP by PIV System

입자영상유속계를 이용한 대형수송함(LPH) 갑판 상부의 유동장 측정 연구

  • Shim, Hojoon (Department of Unmanned and Autonomous Vehicle Engineering, Kyungwoon University) ;
  • Chung, Jindeog (Korea Aerospace Research Institute) ;
  • Cho, Taehwan (Korea Aerospace Research Institute) ;
  • Lee, Seunghoon (Korea Aerospace Research Institute) ;
  • Song, Gisu (Division of Ocean and Ship Engineering, Korea Maritime & Ocean University)
  • 심호준 (경운대학교 무인기공학과) ;
  • 정진덕 (한국항공우주연구원) ;
  • 조태환 (한국항공우주연구원) ;
  • 이승훈 (한국항공우주연구원) ;
  • 송지수 (한국해양대학교 조선.해양개발공학부)
  • Received : 2022.02.19
  • Accepted : 2022.07.18
  • Published : 2022.08.20

Abstract

The flow field measurement above whole area of the flight deck on 'Landing Platform Helicopter (LPH)' was performed by using PIV system in wind tunnel. In various heading angle conditions (0deg, -30deg, -45deg, -60deg, -75deg and ±90deg), the velocity fields such as U velocity & V velocity were measured at three different height above flight deck. Due to the geometrical characteristics of several bodies like deck, crane and super-structure, various vortex were generated. When the heading angle is 0deg, the deck edge vortex by flight deck and massive separation by super-structure were clearly observed by visualization with smoke and PIV, respectively. In other heading angles, the acceleration of flow in space between crane and super-structure were detected. And area with flow separation by super-structure is directly related to the heading angle of vessel.

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Acknowledgement

이 연구는 방위산업기술지원센터로부터 연구비를 지원받아 수행되었음(계약번호 UC200007D).