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소형비행기 가로안정성 향상 및 적합성검증 방안 연구

Study on the lateral stability improvement and compliance verification

  • 최주원 (한국항공우주연구원 비행시험팀) ;
  • 김찬조 (한국항공우주산업주식회사, 공력성능팀) ;
  • 정훈화 (한국항공우주산업주식회사, 공력성능팀) ;
  • 김진수 (한국항공우주산업주식회사, 공력성능팀)
  • 투고 : 2013.06.24
  • 심사 : 2013.06.29
  • 발행 : 2013.06.30

초록

This is a research on the method of how to improve lateral stability for the small general aviation airplane to meet the FAR part 23 requirements. This research is based on the experience of certification flight tests of KC-100 airplane for Korea first type certification. KAS/FAR Part 23.177 is the static lateral and directional stability requirement. And, 23.177(b) requires to show the tendency to raise the low wing in steady heading side slip maneuver. However, it is very difficult for the low wing to be raised at the low speed during the steady heading side slip maneuver. So, the requirement allows not be negative at the $1.2V_{S1}$ speed and takeoff configuration. (static stability requirement requires low wing picked up at any speed except $1.2V_{S1}$ speed and takeoff configuration) In this paper, the static lateral stability requirements and the lessons & learned of KC-100 airplane certification flight test results are shown.

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