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Experimental and Numerical Evaluation of Pressure Gain Combustion in a Rotating Detonation Engine

机译:旋转爆震发动机压力增益燃烧的实验与数值评估

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The detonation structure, pressure gain, and thrust production in a rotating detonation engine (RDE) are studied using a combination of experimental and numerical approaches. High frequency time-dependent and low frequency time-averaged static pressure and thrust measurements are acquired for a range of operating conditions and geometry configurations. Acoustic coupling between the detonation channel and air plenum is important for low air mass flow rates and large air injection slots based on analyses of the pressure measurements in the time and frequency domains. The static pressure increases across the air inlet by up to approximately 15% when utilizing a large air injection slot. The pressure increase across the air inlet demonstrates encouraging progress towards realizing pressure gain combustion in RDEs with corresponding challenges associated with isolating the inlet plenums. The time-dependent pressure measurements acquired using a semi-infinite tube arrangement and time-averaged pressure measurements acquired using a capillary tube attenuated arrangement agree to within 30% depending upon location. Quantification of the similarities and differences between the two techniques represents important progress towards acquiring quantitative time-dependent pressure measurements in the challenging environment presented by RDEs. Two-dimensional simulations of the RDE capture the essential features of the flow field such as the detonation wave height and angle, trailing edge oblique shock wave, shear layer between the freshly and previously detonated products, and deflagration between the fuel fill region and expansion region containing detonated products. The presence of air purging from the plenum to the channel behind the detonation wave is suggested by the comparison of measured and simulated channel pressure distributions. The pressure, thrust, and wave speed measurements provide benchmark data that are useful for evaluating low and high fidelity simulations of RDEs and improving fundamental understanding of the critical design parameters that influence RDE operation and performance.
机译:结合实验和数值方法研究了旋转爆震发动机(RDE)的爆震结构,压力增益和推力产生。针对一系列工作条件和几何形状配置,获取了高频时间相关和低频时间平均的静压力和推力测量值。根据时域和频域中压力测量的分析,引爆通道和空气室之间的声耦合对于低空气质量流量和大空气注入口很重要。当使用大的进气口时,整个进气口的静压力最多可增加15%。进气口的压力增加表明,在实现RDE中的压力增益燃烧方面取得了令人鼓舞的进展,同时面临着与隔离进气室相关的挑战。使用半无限管布置获取的时间相关压力测量值和使用毛细管衰减布置获取的时间平均压力测量值取决于位置,均在30%以内。量化两种技术之间的异同代表了在由RDE提出的具有挑战性的环境中获取定量的,与时间有关的压力测量值方面的重要进展。 RDE的二维模拟捕获了流场的基本特征,例如爆震波的高度和角度,后缘斜向冲击波,新鲜和先前爆燃产品之间的剪切层以及燃料填充区域和膨胀区域之间的爆燃包含引爆产品。比较实测通道压力分布和模拟通道压力分布,表明存在从充气室到爆震波后面通道的空气吹扫。压力,推力和波速测量提供了基准数据,这些数据可用于评估RDE的低保真度和高保真度仿真,以及增进对影响RDE操作和性能的关键设计参数的基本了解。

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