베인형 다기능 대기 자료 센서의 공력 설계

AERODYNAMIC DESIGN OF A VANE TYPE MULTI-FUNCTION AIR DATA SENSOR

  • 박영민 (한국항공우주연구원, 회전익기사업단) ;
  • 최인호 (한국항공우주연구원, 회전익기사업단) ;
  • 이융교 (한국항공우주연구원, 항공기술실) ;
  • 권기정 (한국항공우주연구원, 항공기술실) ;
  • 김성찬 (한국항공우주연구원, 회전익기사업단) ;
  • 황인희 (한국항공우주연구원, 회전익기사업단)
  • 발행 : 2010.05.13

초록

Aerodynamic design of the vane type multi-function probe was tried by using CFD and wind tunnel test for the MALE UAV and small business jets. The present multi-function probe can measure total pressure, static pressure and angle of attack by using rotating vane. Therefore major performances are determined by aerodynamic characteristics of vane. In oder to design the sensor compatible to the requirement, aerodynamic characteristics of sensors was investigated by using CFD and dynamic response analysis was also performed for trasient performance. The final aerodynamic performance was measured by the wind tunnel test at Aeorsonic and the results successfully used for the design of vane type multi-function air data sensor.

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