Journal of the Korea Institute of Military Science and Technology (한국군사과학기술학회지)

The Korea Institute of Military Science and Technology (한국군사과학기술학회)
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Structural Design of pod system for Helicopter Captive Flight Test

헬리콥터 탑재 비행 시험을 위한 파드 시스템 구조 설계

  • Received : 2013.08.02
  • Accepted : 2013.11.15
  • Published : 2013.12.05
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Abstract

The load requirements should be known to design mechanical structure. This paper proposes a generation method of load requirements using U.S. military specification to design the external mounting structure of the helicopters of which the flight environments such as aerodynamic forces and inertia forces are unknown. In this study, the load requirements which were applied at the design of the pod structure for helicopter captive flight test could be computed by using this method. The validation of proposed method was confirmed from the test flight using developed pod system.

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References

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