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http://dx.doi.org/10.9766/KIMST.2013.16.6.779

Structural Design of pod system for Helicopter Captive Flight Test  

Choi, Jang-Seob (ADD)
Publication Information
Journal of the Korea Institute of Military Science and Technology / v.16, no.6, 2013 , pp. 779-788 More about this Journal
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.
Keywords
Military Specification; Helicopter; External Mounting Structure; Design Requirements; Load Analysis; Pod System; Detailed Design; Test Flight;
Citations & Related Records
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