04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY
Y. Zhang¹, H. Zhan¹, B. Mi¹, M. Zhang¹; ¹Northwestern Polytechnical University, China
In this paper, the different factors affecting the separation of aircraft and bombs are studied, and the aeroelasticity under the complicated interfering air flow is considered. This method integrates a set of more comprehensive research and design methods of influencing factors of bomb separation, has high numerical simulation accuracy, and can provide a reference for missile separation design.