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Large Eddy Simulation of early stage aircraft contrails.

机译:早期飞机凝结尾迹的大涡模拟。

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Aircraft contrails at cruise altitudes present a unique problem in atmospheric sciences due to their location where other anthropogenic sources of particulate emissions are absent, and due to their potential impact on the Earth's radiative balance. The scale separation between contrails and atmospheric motions contributes to the large uncertainties in contrail models used in global atmospheric calculations. We study the early-stage contrail growth using high-fidelity Large Eddy Simulations (LES) to better characterize the early contrail-scale processes.; We develop an extended Boussinesq approximation to improve the traditional Boussinesq approximation for inertia-dominated flows with buoyancy. We develop an Eulerian-Lagrangian ice microphysics model and couple it to the flow solver. Verification and validation of the model and the numerical method are discussed. The choice of the number of Lagrangian computational particles required to adequately represent particle statistics is studied.; We investigate the behavior of two dimensional aircraft wakes containing exhaust jets. A mechanism is identified by which the jet-induced baroclinic vorticity influences the wake dynamics. The jets strengthen the primary vorticity and reduce the primary vortex pair spacing, causing accelerated wake descent.; Three-dimensional LES of contrails are carried out for the first 20 second duration of contrail life, starting at 1 second behind the aircraft. The initial conditions at 1 s correspond to a typical large subsonic aircraft. Three different regimes of early contrail growth are found, which are controlled by jet humidity, jet turbulence and ice particle-induced perturbations, and ambient relative humidity with respect to ice (RHi) respectively. Sensitivity of ice properties to atmospheric temperature and relative humidity, initial ice nuclei size and number density is characterized. Ambient temperature and RHi are found to be critical in determining the rate of ice growth. Particle size distribution is skewed to higher radii for higher RHi. The total ice area, ice particle size, and number density are found to be sensitive to the initial ice nuclei number density, but the total ice mass remains insensitive to it at least in the regime considered. Ice growth is found to be relatively insensitive to the initial particle size for the size range considered.
机译:飞机在巡航高度上的凝结尾迹在大气科学中是一个独特的问题,这是因为它们的位置不存在其他人为的颗粒物排放源,并且它们可能会对地球的辐射平衡产生影响。轨迹转换和大气运动之间的尺度分离为全球大气计算中使用的轨迹转换模型带来了很大的不确定性。我们使用高保真大涡模拟(LES)研究了早期的轨迹转换过程,以更好地描述早期的轨迹转换过程。我们开发了扩展的Boussinesq逼近,以改进具有浮力的惯性主导流的传统Boussinesq逼近。我们开发了一个欧拉-拉格朗日冰微物理模型,并将其耦合到流动求解器。讨论了模型和数值方法的验证和确认。研究了充分代表粒子统计量所需的拉格朗日计算粒子数的选择。我们调查了包含排气喷嘴的二维飞机尾流的行为。确定了一种机制,通过该机制喷射引起的斜压涡旋会影响尾流动力学。喷流增强了初级涡旋并减小了初级涡旋对的间距,导致加速了尾流下降。转换轨迹的三维LES在转换轨迹寿命的前20秒内执行,从飞机后1秒开始。 1 s的初始条件对应于典型的大型亚音速飞机。发现了三种不同的早期轨迹转换方式,分别由射流湿度,射流湍流和冰粒引起的扰动以及相对于冰的环境相对湿度(RHi)控制。表征了冰性质对大气温度和相对湿度,初始冰核尺寸和数密度的敏感性。发现环境温度和RHi对确定冰的生长速度至关重要。粒径分布偏向较高的半径以获得较高的RHi。发现总冰面积,冰粒径和数密度对初始冰核数密度敏感,但是至少在所考虑的方案中总冰量对其保持不敏感。对于所考虑的尺寸范围,发现冰的生长对初始粒径相对不敏感。

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