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

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Extended Beam Analysis for Compound Rotorcraft Fuselage Design

복합형 회전익 항공기 동체 설계를 위한 확장된 보 해석

  • Park, Sunhoo (Department of Aerospace Engineering, Seoul National University) ;
  • Im, Byeonguk (Department of Aerospace Engineering, Seoul National University) ;
  • Chun, TaeYoung (Department of Aerospace Engineering, Seoul National University) ;
  • Yeom, Jewan (Department of Aerospace Engineering, Seoul National University) ;
  • Shin, SangJoon (Department of Aerospace Engineering, Seoul National University)
  • Received : 2020.07.03
  • Accepted : 2020.08.18
  • Published : 2020.09.01
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Abstract

This paper describes an improved beam analysis for compound rotorcraft fuselage design. The present beam approach is capable of analyzing fuselage composed of stiffeners using equivalent layer methodology. Thickness of the skin and laminated layer approach are suggested based on the unified beam formulation. The analysis which considers an equivalent stiffener layer is performed for a fuselage with stiffeners and preliminary study about the specification of stiffeners is conducted and compared by the results using the existing software.

본 연구에서는 복합형 회전익 항공기 동체의 설계를 위해 확장된 보 해석을 기술한다. 개발된 보 접근 방법은 등가 보강재 층 방법을 사용하여 보강재로 구성된 동체의 해석이 가능하다. 통합 정식화 보 이론에 기반하여 외피의 두께 및 적층 고려 방법을 제시하였다. 보강재가 고려된 동체에 대해 등가 보강재 층 방법을 적용하여 해석을 수행하였고, 보강재의 제원에 관한 예비 연구 결과를 도출하였으며 상용 프로그램을 이용하여 검증 및 비교를 수행했다.

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