Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Scaling Methods for Icing Wind Tunnel Test

결빙 풍동시험을 위한 스케일링 기법 연구

  • 안영갑 (국방기술품질원 사천센터) ;
  • 명노신 (경상대학교 항공우주시스템공학과 및 항공기부품기술연구소)
  • Received : 2011.10.05
  • Accepted : 2012.01.13
  • Published : 2012.02.01
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Abstract

In-flight icing remains as one of the most persistent hazards for aircraft operations. The effect of icing on aircraft performance and safety has to be evaluated during the development and airworthiness certification process. The scaling method is a procedure to determine the scaled test conditions in icing wind tunnels in order to produce the same result as when the reference model is exposed to the desired cloud conditions. In this study, a scaling program is developed to provide an easy-to-use tool to the aero-icing community. The Olsen and Ruff 4th methods are employed for this purpose and the velocity is calculated by matching the dimensionless Weber number. To validate the program, the results are compared with the NASA scaling results. The scaling examples based on FAR (Federal Aviation Regulation) Part 25 Appendix C are also presented. Finally, a validation study using a state-of-the-art icing simulation code FENSAP-ICE is presented.

비행 중 결빙은 항공기 운용에 위험한 상황을 초래하게 되며, 개발 및 감항 인증 과정중 성능과 안전에 미치는 영향이 평가되어야 한다. 평가를 위한 결빙 풍동시험에서 스케일링 기법은 실제와 동등한 수집율과 결빙량이 모사되는 대체시험 조건을 결정하는 기법이다. 본 논문에서는 Olsen 및 Ruff-IV 기법과 무차원 Weber 수를 일치시켜 속도를 계산하는 방법을 적용하여 연구자들이 쉽게 이용할 수 있도록 스케일링 프로그램을 개발하였다. 동일조건에서 수행된 NASA 스케일링 결과와 비교하여 프로그램을 검증하였다. 또한 FAR Part 25 Appendix C를 적용한 스케일링 사례를 제시하고 결빙코드 FENSAP-ICE를 이용하여 스케일링 기법을 검증하였다.

Keywords

References

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