Wavelet optical flow velocimetry of a scramjet combustor using high-speed frame-straddling focusing schlieren images

IF 5.8 2区 工程技术 Q2 ENERGY & FUELS
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引用次数: 0

Abstract

Scramjet combustors feature ultra-high-speed turbulent reacting flows with high temperatures and intense luminescence. Measurement of velocity fields under such extreme conditions presents great challenges. The present work demonstrated a seedless velocimetry approach using focusing schlieren images (FSIs) of high spatiotemporal resolution in a scramjet engine. Two fuel mass flow rates (Case1 and Case2) were investigated with corresponding global equivalence ratios of 0.27 and 0.13, respectively. The FSIs enabled by the employment of a high-speed pulsed LED light source are characterized by an effective exposure of 100 ns, and a 500-ns frame-straddling time interval with full resolution of 1280 × 800 pixels recorded at 76 kHz. The 100-ns exposure allows for capturing of transient high-speed flow motion without blurring, and the 500-ns time interval ensures an appropriate spatiotemporal correlation between subsequent schlieren images for high-speed reacting flows. A wavelet-based optical flow velocimetry (wOFV) algorithm was developed and applied to the FSIs. In contrast to the correlation-based algorithms widely employed in PIV for distinct particles, the wOFV algorithm suits better FSIs with continuous variation in brightness. The maximal velocities in the main duct of the scramjet combustor were measured to be approximately 550 m s-1 and 1100 m s-1 for Case 1 and Case2, suggestively corresponding to subsonic and supersonic combustion modes, respectively. The measured velocity inside the cavity is generally below 200 m s-1 for both cases. Recirculation regions and their dynamic motions inside the cavity were well resolved. In summary, the development of the novel velocimetry approach holds great potential for applications in extreme flow conditions.

Novelty and Significance Statement

: Present work demonstrates a seedless velocimetry approach based on high-speed frame-straddling focusing schlieren imaging coupled with the novel wavelet optical flow velocimetry (wOFV) algorithm. Velocity field measurement realized in a scramjet combustor with high spatiotemporal resolution (1280 × 800 pixels at 38 kHz) for the first time, showing great abilities to accommodate wide velocity range and to resolve dynamic flow characteristics with potentials for broader future applications.

利用高速跨帧聚焦雪莲花图像对扰动喷气燃烧器进行小波光学流速度测量
Scramjet 燃烧器具有超高速湍流反应流,温度高,发光强。在这种极端条件下测量速度场是一项巨大的挑战。本研究展示了一种无籽测速方法,该方法在争气式喷气发动机中使用了高时空分辨率的聚焦裂隙成像(FSI)。研究了两种燃料质量流量(Case1 和 Case2),相应的全局当量比分别为 0.27 和 0.13。利用高速脉冲 LED 光源实现的 FSI 的特点是有效曝光时间为 100 ns,帧跨时间间隔为 500 ns,以 76 kHz 的频率记录 1280 × 800 像素的全分辨率。100 毫微秒的曝光时间可捕捉瞬时高速流动运动而不会模糊,500 毫微秒的时间间隔可确保高速反应流的后续舍利连图像之间具有适当的时空相关性。我们开发了一种基于小波的光学流动测速(wOFV)算法,并将其应用于 FSIs。与 PIV 中广泛使用的基于相关性的算法相比,wOFV 算法更适合亮度连续变化的 FSI。在情况 1 和情况 2 中测量到的扰流喷气燃烧器主风道中的最大速度分别约为 550 m s-1 和 1100 m s-1,这表明分别对应于亚音速和超音速燃烧模式。在这两种情况下,空腔内的测量速度一般都低于 200 m s-1。空腔内的再循环区域及其动态运动得到了很好的解析。总之,新型测速方法的开发为极端流动条件下的应用提供了巨大潜力:目前的工作展示了一种基于高速跨帧聚焦裂隙成像和新型小波光流测速(wOFV)算法的无籽测速方法。首次以高时空分辨率(1280 × 800 像素,38 kHz)在扰流喷气燃烧器中实现了速度场测量,显示了适应宽速度范围和解析动态流动特性的强大能力,为未来更广泛的应用提供了可能性。
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来源期刊
Combustion and Flame
Combustion and Flame 工程技术-工程:化工
CiteScore
9.50
自引率
20.50%
发文量
631
审稿时长
3.8 months
期刊介绍: The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on: Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including: Conventional, alternative and surrogate fuels; Pollutants; Particulate and aerosol formation and abatement; Heterogeneous processes. Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including: Premixed and non-premixed flames; Ignition and extinction phenomena; Flame propagation; Flame structure; Instabilities and swirl; Flame spread; Multi-phase reactants. Advances in diagnostic and computational methods in combustion, including: Measurement and simulation of scalar and vector properties; Novel techniques; State-of-the art applications. Fundamental investigations of combustion technologies and systems, including: Internal combustion engines; Gas turbines; Small- and large-scale stationary combustion and power generation; Catalytic combustion; Combustion synthesis; Combustion under extreme conditions; New concepts.
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