A Kinematic Study of Individual Rotating Detonation Engine Waves Using K-means Algorithm

Taha Rezzag, R. Burke, K. Ahmed
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Abstract

The current research is concerned with studying the instantaneous properties of the detonation waves in a RDRE by tracking each individual wave and recording its position, velocity, and peak intensity as it travels around the annulus. This information is retrieved by a non-intrusive method consisting of using a data mining technique, the k-means algorithm, to distinguish each detonation from each other in a particular frame. An algorithm was then developed to match the detonations of a current frame to the ones of a previous frame. The code was validated against results found from the back-end imaging method developed by the Air Force Research Laboratory with excellent agreement. Results for two and three-wave mode cases show that the instantaneous detonation wave speeds oscillate around the mode locked average wave speed computed from a detonation surface. Moreover, the investigation of the relationship of the detonation’s peak light intensity with the azimuthal position revealed to also be oscillatory but more distinct.
基于k -均值算法的单个旋转爆震发动机波的运动学研究
目前的研究是通过跟踪每一个单独的波,记录它在环空传播时的位置、速度和峰值强度,来研究rdrre中爆震波的瞬时特性。该信息通过非侵入式方法检索,该方法使用数据挖掘技术,即k-means算法,以区分特定帧中的每个爆炸。然后开发了一种算法,将当前帧的爆炸与前一帧的爆炸相匹配。该代码与空军研究实验室开发的后端成像方法的结果进行了验证,结果非常一致。两波和三波模态的结果表明,瞬时爆轰波速度在爆轰面计算的锁定模态平均波速度附近振荡。此外,对爆轰峰光强与方位角的关系的研究表明,爆轰峰光强与方位角的关系也是振荡的,但更为明显。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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