AERODYNAMIC DESIGN OF A MULTI-FUNCTION AIR DATA SENSOR BY USING CFD AND WIND TUNNEL TEST
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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) |
1 | 1985, Wickens, R.H. and Williams, C.D., "Calibration and Use of Five-hole Flow Direction Probes for Low Speed Wind Tunnel Application," Aeronautical Note, National Research Council, Canada, p.49. |
2 | 2009 Kang, Y., Kim, S., Myong, R., Cho, T., Park, Y. and Choi, I., "Calibration of a Five-hole Multi-function Probe for Helicopter Air Data Sensors," International Journal of Aeronautical & Space Sciences, Vol.10, No.2, pp.43-61. 과학기술학회마을 DOI |
3 | 1994, Hagen, F.W. and Seidel, H, "Deutsche Airbus Flight Test of Rosemount Smart Probe for Distributed Air Data Systems," Aerospace and Electronic Systems Magazine, Vol.9, Issue 4. |
4 | http://www.sensors.goodrich.com |
5 | http://www.thalesgroup.com |
6 | http://www.aerosonic.com |
7 | 2009, Performance-Based Specification for the Multi- Function Intelli-Probe, KARI Internal Document. |
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