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AERODYNAMIC DESIGN OF A MULTI-FUNCTION AIR DATA SENSOR BY USING CFD AND WIND TUNNEL TEST  

Park, Y.M. (한국항공우주연구원, 회전익기사업단)
Choi, I.H. (한국항공우주연구원, 회전익기사업단)
Lee, Y.G. (한국항공우주연구원, 항공기술실)
Kwon, K.J. (한국항공우주연구원, 항공기술실)
Kim, S.C. (한국항공우주연구원, 회전익기사업단)
Hwang, I.H. (한국항공우주연구원, 회전익기사업단)
Publication Information
Journal of computational fluids engineering / v.15, no.3, 2010 , pp. 32-38 More about this Journal
Abstract
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 order to design the sensor compatible to the requirement, aerodynamic characteristics of sensors were investigated by using CFD and dynamic response analysis was also performed for transient performance. The final aerodynamic performance was measured by the wind tunnel test at Aerosonic and the results were compared with the present design. The results showed that the aerodynamic design using the CFD can be successfully used for the design of vane type multi-function air data sensor.
Keywords
Aerodynamic Design; Multi-function; Air Data Sensor;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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