대한건축학회논문집:구조계 (Journal of the Architectural Institute of Korea Structure & Construction)

대한건축학회 (Architectural Institute of Korea)
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미사일-타깃 상호작용해석법에 의한 대형항공기 충돌해석을 위한 항공기 충돌하중이론 및 질량분포 결정

Aircraft Impact Theory and Mass Model for the Missile-Target Interaction Analysis of Large Aircraft

  • 투고 : 2013.05.29
  • 발행 : 2013.10.25
⟨ 이전 논문 다음 논문 ⟩

초록

In this paper, we model the total mass and mass distribution to simulate the missile-target interaction analysis of aircraft. And the difference of mass of fuel was also considered, because it is about 40 percent of total mass when it is full-filled. The aircraft FE model was developed by determining mass distribution. And aircraft FE model was verified by impact analysis simulated by AUTODYN. Through the developed aircraft FE model, the impact on the various surface of target, which cannot be analyzed by Riera model, can be analyzed by the missile-target interaction analysis. The large commercial B747 aircraft was used for the missile which is using for long distance flight. To determine the mass model of aircraft, the Riera approach was used for the reference impact time history graphs which provided by OECE-NEA (2002) and Arros and Doumbalski (2007).

키워드

과제정보

연구 과제 주관 기관 : 한국연구재단

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