CAJ | 학술논문

提出了一种新的折叠弹翼悬挂物机弹分离轨迹试验技术，重点解决了在机弹分离过程中折叠弹翼动态展开时悬挂物的气动力获取问题。研究表明，提出的试验技术通过将悬挂物气动力修正方法引入到悬挂物分离安全性研究当中，准确地得到悬挂物的分离特性，解决了折叠弹翼悬挂物分离轨迹风洞试验技术瓶颈，为折叠弹翼悬挂物的投放分离安全性提供一套工程实用的解决方案。
제출료일충신적절첩탄익현괘물궤탄분리궤적시험기술，중점해결료재궤탄분리과정중절첩탄익동태전개시현괘물적기동력획취문제。연구표명，제출적시험기술통과장현괘물기동력수정방법인입도현괘물분리안전성연구당중，준학지득도현괘물적분리특성，해결료절첩탄익현괘물분리궤적풍동시험기술병경，위절첩탄익현괘물적투방분리안전성제공일투공정실용적해결방안。
The folding wing has a dynamic unfolding process during aircraft&store separa-tion,which will cause an evident change in aerodynamic characteristics of the store and further result in difficulty of acquiring the correct separation characteristics of the store by using the con-ventional CTS WTT (Captive Trajectory Simulation Wind Tunnel Test).Therefore,a new test technique is put forward for CTS WTT of store with folding wing,and emphasizes on obtaining aerodynamic data of stores at wings spreading during aircraft&store separation.The technical difficulty involved in this research is to establish the simulation method for the dynamic unfolding process of the folding wing,and its key point is the formation principle for the aerodynamic force of the store,That is both under the aircraft disturbance flow condition with the same location and same attitude angle.The store’s aerodynamic force when the wing is unfolded is the aerodynamic force when the wing is folded added with the aerodynamic difference of free flow between the un-folding and folding statuses of the wing.The whole testing method and procedure are introduced, and details in the procedures of the ground bench test,the establishment of parameter database for the unfolding status of the folding wing,the establishment of aerodynamic database for differ-ent statuses of the folding wing,and the aerodynamic coefficient corrective calculation of trajecto-ry calculation in relevant tests were presented.Then the technique was validated with the folding wing weapon on some light fighter.