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D-SEND PROJECT FOR LOW SONIC BOOM DESIGN TECHNOLOGY

机译:低声振设计技术的D-SEND项目

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The D-SEND project aims to demonstrate the feasibility of JAXA 's low sonic boom design concept through the balloon drop tests. The project is carried out in two phases (D-SEND#1 and D-SEND#2). The D-SENDM drop tests were conducted twice in May 2011. The two different axisymmetric bodies were dropped from the balloon at 30km altitude and the conventional N-type and the shaped sonic booms were successfully captured by microphones at multiple altitudes up to lkm. The D-SEND#2 is scheduled to be conducted in 2013 in the same way as the D-SENDttl. An unmanned experimental supersonic airplane based on the JAXA's low sonic boom design technology is newly designed. The sonic boom intensity of the airplane is designed to be almost as half as the conventional supersonic transport. The airplane autonomously flies over microphones and the shaped sonic booms are measured. In this paper, the balloon drop test method, the test bodies and the aerial sonic boom measurement system with blimps are described. Some test results of the D-SEND#1 are presented as well.
机译:D-SEND项目旨在通过气球坠落测试证明JAXA的低声波吊臂设计概念的可行性。该项目分两个阶段进行(D-SEND#1和D-SEND#2)。 D-SENDM跌落测试在2011年5月进行了两次。两个不同的轴对称物体在30 km的高度从气球上掉落,并且常规的N型和异型声波吊臂在长达1 km的多个高度成功通过麦克风捕获。 D-SEND#2计划于2013年进行,其方式与D-SENDttl相同。新设计了一种基于JAXA低声波吊臂设计技术的无人实验性超音速飞机。飞机的音爆强度设计成几乎是传统超音速传输的一半。飞机自动飞过麦克风,并测量成形的声波吊杆。本文介绍了气球坠落测试方法,测试体和带有飞艇的空中声波臂测量系统。还介绍了D-SEND#1的一些测试结果。

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