항공기용 자왜진동형 결빙감지센서의 부착 위치에 따른 결빙성장 전산해석 = COMPUTATIONAL ANALYSIS OF ICE ACCRETION ON MAGNETOSTRICTIVE IN-FLIGHT ICING DETECTION SENSOR DEPENDING ON ATTACHMENT POSITION

다국어 초록 (Multilingual Abstract)

Magnetostrictive ice detection sensor detects ice accretions that occur on the surface of the aircraft by measuring the change in frequency according to the amount of ice freezing that grows on the probe surface. In this study, computational approach is used to study and analyze the effects of sensor attachment position on the aspects of freezing that occur on the ice detection sensor probe by changing the wall boundary conditions such as the shape of the face on which the sensor is attached and whether the boundary layer is formed or not.

참고문헌 (Reference)

1 안영갑, "결빙 풍동시험을 위한 스케일링 기법 연구" 한국항공우주학회 40 (40): 146-156, 2012

2 SAE International, "Minimum Operational Performance Specification for Inflight Icing Detection Systems"

3 정성기, "KC-100 항공기의 표면발생 Icing 형상 및 공력 영향성 연구" 한국항공우주학회 38 (38): 530-536, 2010

4 Ministry of Land, "Infrastructure and Transport Republic of Korea, Korean Airworthiness Standards"

5 Muhammad, S. V., "Ice accretion on circular cylinder in relation to its diameter" 4 : 55-61, 2016

6 Bourgault, Y, "Development of a Shallow-Water Icing Model in FENSAP-ICE" 37 (37): 2000

7 Muhammad, A., "Determination of Water Droplet Collection Efficiency: An Empirical Model" 2017

8 Anderson, D, "Characterization of ice roughness from simulated icing encounters" 1997

9 Muhammad, S. V., "Atmospheric Ice Accretion on Non-Rotating Circular Cylinder" 3 (3): 197-205, 2011

10 Ansys.Inc, "Ansys Fensap-Ice User manual"

11 Federal Aviation Administration, "Advisory Circular, No.20-73A"