An evaluation criterion of aircraft-store compatibility for internal weapons separation is put forward and the drop tests are conducted in a high-speed wind tunnel with the Mach 1.5. The dynamic store models are designed by light Mach scaling (LMS) and are released to the freestream by an ejection mechanism driven by the high-pressure air from two rectangular cavities with a length-to-depth ratio of 7.76 and 11.86. The three affected factors of initial pitch angle, angle-of-attack of aircraft and length-to-depth ratio are considered and analysed. The result of the drop tests shows the aircraft-store compatibility of the internal weapons decreases along with increasing AOA of carrier aircraft and even changes from compatibility to incompatibility. The flow characteristics of the cavity have a great influence on the aircraft-store compatibility of internal weapons separation. The compatibility of aircraft-store separation tends to obviously decrease when the cavity change from open to transitional cavity flow. The initial pitch angle of the store is the key factor affecting the aircraft-store compatibility. With the increase of initial pitch angle, the aircraft-store compatibility of is obviously reduced, even unsafe.

提出了一种用于内部武器分离的飞机商店兼容性的评估标准，并在1.5马赫的高速风洞中进行了跌落测试。动态存储模型是通过轻马赫缩放比例（LMS）设计的，并通过喷射机构释放到自由流，该喷射机构是由高压空气从两个矩形腔体中驱动的，这些腔体的长深比为7.76和11.86。考虑并分析了初始俯仰角，飞机攻角和长深比这三个影响因素。跌落试验的结果表明，内部武器的飞机商店兼容性随着舰载飞机的AOA的增加而降低，甚至从兼容性变为不兼容性。空腔的流动特性对内部武器分离的飞机商店兼容性具有很大的影响。当空洞从开放流转变为过渡空洞时，飞机与飞机之间的分离兼容性会明显降低。机库的初始俯仰角是影响飞机机库兼容性的关键因素。随着初始俯仰角的增加，飞机与飞机的兼容性明显降低，甚至不安全。