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在FL-13风洞对起落架主要元件和某机主起落架进行了吹风试验研究,在此基础上,讨论了确定起落架主要元件气动力系数的影响因素。为起落架收放气动载荷计算提供了依据。
In the FL-13 wind tunnel, the main components of landing gear and some main landing gear were studied. Based on this, the influencing factors for determining the aerodynamic coefficient of main components of landing gear were discussed. The retractable landing gear provided the basis for aerodynamic load calculation.