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http://dx.doi.org/10.12985/ksaa.2011.19.4.067

Flight Loads Analysis for Conceptual Study of the Regional Aircraft Wing Structure  

Shin, Jeong-Woo (충남대학교 대학원 기계설계공학과)
Kang, Wang-gu (한국항공우주연구원 항공체계실)
Kim, Sung-Joon (한국항공우주연구원 항공구조팀)
Hwang, In-Hee (한국항공우주연구원 항공구조팀)
Publication Information
Journal of the Korean Society for Aviation and Aeronautics / v.19, no.4, 2011 , pp. 67-73 More about this Journal
Abstract
For loads analysis of airplane, applicable regulation should be determined. Then, loads conditions are prepared from the regulation. Modeling for aerodynamic, mass, and structure are performed. Panel method is usually adopted for aircraft loads analysis to obtain air loads. The ARGON which is a multidisciplinary fixed wing aircraft design software co-developed by the KARI and TsAGI are used for loads analysis. The ARGON can be utilized for flutter and stress analysis as well as for flight and ground loads analysis. In this paper, flight loads analysis for wing structural design of the regional aircraft at the conceptual design phase are performed with the ARGON. FAR 25 is used for the regulation for the load analysis. Shear force, bending moment and torsion diagrams for the wing and shear force and hinge moment for the aileron are presented.
Keywords
Flight Loads; FAR; Panel Method; ARGON; Regional Aircraft;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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