Inhibition of the oblique detonation wave detachment in two-phase n-heptane/air mixtures

IF 5.8 2区 工程技术 Q2 ENERGY & FUELS
Hongbo Guo , Yue Sun , Ruixuan Zhu , Shuo Wang , Majie Zhao , Baolu Shi , Xiao Hou
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引用次数: 0

Abstract

In this work, oblique detonation wave propagations in n-heptane droplet/vapor/air mixtures induced by a wedge at high altitude and Mach number are simulated by the Eulerian-Lagrangian method with a skeletal chemical mechanism. This work is a first attempt to inhibit the detachment of oblique detonation wave (ODW) and expand the operation range of thrusters based on oblique detonation combustion in partially pre-vaporized n-heptane/air mixtures. Effects of gas/liquid equivalence ratios and droplet diameters are considered, and the ODW morphology is analyzed. Standing windows, ODW characteristics and predictability of detachment inhibition are discussed. First, the detonation theoretical calculation is performed at 25–40 km operation conditions for pure gas n-heptane/air mixtures. The results show that the wedge angle range for successful ignition, i.e., standing window, increases with the increase of flight altitude and Mach number. The internal energy and kinetic energy of mixtures are affected by the wedge angle and flight Mach number, so that the maximum angle of ODW with flight conditions presents an opposite trend over or below Mach 10. The two-dimensional (2D) ODWs in our simulation scope, which are triggered by the collision of the initiation zones formed from the wedge, show a multi-wave head structure similar to normal detonation. Detachment is inhibited in partially pre-vaporized n-heptane/air mixtures, due to the non-explosive mixtures near triple-point and the post-ODW inter-phase mass and energy transfers by the latent heat absorption and vapor addition from droplet evaporation. Moreover, the predictability of pre-vaporized n-heptane on inhibiting ODW detachment is explored through the relationship of chemical and evaporation timescales. It is demonstrated that the excitation time is very small approaching the detachment condition where an abrupt ODW tends to form. Accordingly, when the ratio of droplet heat absorption time to evaporation time is relatively high, i.e., τh / (τev)1/2 > 0.01, the ODW detachment is more likely to be inhibited.
抑制正庚烷/空气两相混合物中的斜向爆轰波脱落
在这项工作中,利用欧拉-拉格朗日方法和骨架化学机制,模拟了在高海拔和高马赫数下由楔子诱发的正庚烷液滴/蒸汽/空气混合物中的斜爆轰波传播。这项工作首次尝试抑制斜爆波(ODW)的脱离,并扩大了基于部分预汽化正庚烷/空气混合物中斜爆燃烧的推进器的工作范围。考虑了气/液当量比和液滴直径的影响,并分析了 ODW 形态。讨论了驻留窗口、ODW 特性和脱离抑制的可预测性。首先,对纯气体正庚烷/空气混合物在 25-40 km 运行条件下进行了爆轰理论计算。结果表明,成功点火的楔角范围,即驻留窗口,随着飞行高度和马赫数的增加而增大。混合物的内能和动能受楔角和飞行马赫数的影响,因此 ODW 的最大角度与飞行条件呈相反趋势,超过或低于 10 马赫。在我们的模拟范围内,二维(2D)ODWs 由楔形形成的起爆区碰撞触发,显示出与正常起爆类似的多波头结构。在部分预汽化的正庚烷/空气混合物中,由于三重点附近的非爆炸性混合物以及ODW后相间的质量和能量转移(由液滴蒸发产生的潜热吸收和蒸汽添加),分离受到抑制。此外,还通过化学和蒸发时间尺度的关系,探讨了预蒸发正庚烷对抑制 ODW 脱离的可预测性。结果表明,在接近分离条件时,激发时间非常小,在此条件下往往会形成突然的 ODW。因此,当液滴吸热时间与蒸发时间之比相对较高时(即 τh / (τev)1/2 > 0.01),ODW 脱离更容易受到抑制。
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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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