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Stabilization and structure of N-heptane flame on CWJ-spray burner with kHZ SPIV and OH-PLIF

机译:具有kHZ SPIV和OH-PLIF的CWJ喷雾燃烧器上正庚烷火焰的稳定和结构

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摘要

A curved wall-jet (CWJ) burner was employed to stabilize turbulent spray flames that utilized a Coanda effect by supplying air as annular-inward jet over a curved surface, surrounding an axisymmetric solid cone fuel spray. The stabilization characteristics and structure of n-heptane/air turbulent flames were investigated with varying fuel and air flow rates and the position of pressure atomizer (L). High-speed planar laser-induced fluorescence (PLIF) of OH radicals delineated reaction zone contours and simultaneously stereoscopic particle image velocimetry (SPIV) quantified the flow field features, involving turbulent mixing within spray, ambient air entrainment and flame-turbulence interaction. High turbulent rms velocities were generated within the recirculation zone, which improved the flame stabilization. OH fluorescence signals revealed a double flame structure near the stabilization edge of lifted flame that consisted of inner partially premixed flame and outer diffusion flame front. The inner reaction zone is highly wrinkled and folded due to significant turbulent mixing between the annular-air jet and the fuel vapor generated from droplets along the contact interface of this air jet with the fuel spray. Larger droplets, having higher momentum are able to penetrate the inner reaction zone and then vaporized in the low-speed hot region bounded by these reaction zones; this supports the outer diffusion flame. Frequent local extinctions in the inner reaction zone were observed at low air flow rate. As flow rate increases, the inner zone is more resistant to local extinction despite of its high wrinkling and corrugation degree. However, the outer reaction zone exhibits stable and mildly wrinkled features irrespective of air flow rate. The liftoff height increases with the air mass flow rate but decreases with L.
机译:弯曲壁面喷射(CWJ)燃烧器用于稳定湍流喷雾火焰,利用柯恩达效应,该空气通过将空气作为环形向内喷射流提供在弯曲表面上,并围绕轴对称固体圆锥形燃料喷雾而产生。研究了正庚烷/空气湍流火焰在不同燃料和空气流量以及压力雾化器(L)位置变化下的稳定特性和结构。 OH自由基的高速平面激光诱导荧光(PLIF)描绘了反应区的轮廓,同时立体粒子图像测速(SPIV)量化了流场特征,涉及喷雾内的湍流混合,环境空气夹带和火焰-湍流相互作用。在再循环区内产生了高湍流均方根速度,从而改善了火焰稳定性。 OH荧光信号揭示了在提升火焰稳定边缘附近的双重火焰结构,该结构由内部部分预混火焰和外部扩散火焰前沿组成。由于环形空气射流与由液滴产生的燃料蒸气之间的剧烈湍流混合,沿着该空气射流与燃料喷雾的接触界面,内部反应区高度起皱和折叠。具有较高动量的较大液滴能够穿透内部反应区,然后在这些反应区所限制的低速热区中蒸发。这支撑了外部扩散火焰。在低空气流速下,观察到内部反应区中的频繁局部灭绝。随着流速的增加,尽管内部区域起皱和起皱程度较高,但其对局部灭绝的抵抗力更大。但是,无论空气流速如何,外部反应区均表现出稳定且轻度起皱的特征。升空高度随空气质量流量而增加,但随L减小。

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