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一、引言为研究军用飞机强度和刚度规范,试飞研究中心按航空部“六五”研究规划要求,进行了歼某飞机尾翼机动载荷试飞测量研究,得到了具有重要价值的飞行试验结果。本文就纵向机动试飞的操纵方法及强度规范中的有关规定,粗浅地谈谈看法.
I. INTRODUCTION In order to study the specifications of the strength and stiffness of military aircraft, the Research Center for Flight Test conducted a pilot study on the test flight of a certain aircraft tail rotor according to the requirements of the “6th Five-Year Plan” of the Ministry of Aviation and obtained the flight test results of great value. This article talks about the maneuvering method of longitudinal maneuver test and the relevant provisions in the strength code.