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高速飞行器燃油瞬态温度预测的修正热网络法
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作者 程显达 郑皓冉 +1 位作者 杨学森 董威 《上海交通大学学报》 EI CAS CSCD 北大核心 2023年第6期728-738,共11页
针对高速飞行器燃油消耗全阶段温度场三维瞬态计算存在效率过低问题,为满足高速飞行器燃料系统快速迭代设计过程中燃油温度场计算的需求,通过在热传导方程中添加掺混系数表征燃油内部热对流,在热平衡方程中添加传质项表征燃油宏观流动,... 针对高速飞行器燃油消耗全阶段温度场三维瞬态计算存在效率过低问题,为满足高速飞行器燃料系统快速迭代设计过程中燃油温度场计算的需求,通过在热传导方程中添加掺混系数表征燃油内部热对流,在热平衡方程中添加传质项表征燃油宏观流动,提出一种满足设计精度的高效修正热网络方法.基于提出的热网络法构建高速飞行器储油系统瞬态热分析模型,在不同的热边界条件和储油系统几何结构下,该热网络法计算结果与计算流体动力学(CFD)方法结果的偏差低于5%,计算效率极大提高.采用CFD计算与修正热网络法结合的方式,为高速飞行器燃料储存系统设计提供了新的燃油瞬态温度变化预测方法. 展开更多
关键词 高速飞行器燃油系统 瞬态温度预测 修正热网络法 传热
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应用过程神经网络的航天器瞬态温度预测方法 被引量:1
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作者 陈冠宇 杨森 +3 位作者 彭威 多乐乐 张健鹏 刘宪闯 《航天器工程》 CSCD 北大核心 2023年第6期25-30,共6页
航天器在轨温度受空间热环境影响变化较大,同时研制阶段的热分析与热试验往往也耗时较长,因此通过准确有效的预测方法为其提供在轨温度预警信息、提高热仿真与热试验效率至关重要。文章提出航天器瞬态温度预测方法,依据航天器在轨温度... 航天器在轨温度受空间热环境影响变化较大,同时研制阶段的热分析与热试验往往也耗时较长,因此通过准确有效的预测方法为其提供在轨温度预警信息、提高热仿真与热试验效率至关重要。文章提出航天器瞬态温度预测方法,依据航天器在轨温度实测数据,采用相空间重构理论构建样本集完成训练,应用过程神经网络建立瞬态温度预测模型,并对温度进行外推预测。经验证,根据温度预测方法建立的温度预测模型绝对误差最大值为0.746 K,可在满足工程精度的情况下实现对航天器瞬态温度的快速预测。 展开更多
关键词 航天器瞬态温度预测 过程神经网络 相空间重构理论
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Alternate Form of Damped Wave Conduction and Relaxation Equation a Capite Adcalcem in Temperature
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作者 Kal Renganathan Sharma 《Journal of Physical Science and Application》 2013年第1期46-53,共8页
An alternate non-Fourier heat conduction equation is derived from consideration of translation motion of spinless electron under a driving force due to an applied temperature gradient. This equation is a eapite ad cal... An alternate non-Fourier heat conduction equation is derived from consideration of translation motion of spinless electron under a driving force due to an applied temperature gradient. This equation is a eapite ad calcem,temperature. Elimination of the rate of change of velocity with respect to time leads to a non-Fourier heat conduction equation with a accumulation of temperature or ballistic term in it. The new constitutive heat conduction equation is combined with the energy balance equation in one dimension. The governing equation for transient temperature a partial differential equation (Eq. (23)) is solved for by the method of Laplace transforms. The problem considered is the semi-infinite medium with constant thermo physical properties with constant wall temperature boundary condition. A closed form analyticalexpression for the transient temperature was obtained (Eq. (36)) after truncation of higher order terms in the infinite binomial series and use of convolution and lag properties. This solution is compared with that obtained using the parabolic Fourier model and the damped wave model as presented in an earlier study. The predictions of Eq. (36) are closer to the Fourier model. The convex nature of the temperature curve is present. 展开更多
关键词 Transport theory non-fourier conduction CWT constant wall temperature binomial infinite series.
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Transient emission wavelength estimation for DFB laser with temperature tuning 被引量:1
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作者 李金义 乔琛智 +1 位作者 宋丽梅 郭庆华 《Optoelectronics Letters》 EI 2017年第2期108-112,共5页
The prediction method of dynamic wavelength is proposed for temperature tuning process. The temperature of the thermistor integrated in laser diode(LD) module is recorded to predict the LD chip temperature. Then accor... The prediction method of dynamic wavelength is proposed for temperature tuning process. The temperature of the thermistor integrated in laser diode(LD) module is recorded to predict the LD chip temperature. Then according to the injection current and priori tuning characteristics of the LDs, the emission wavelength is estimated in real time. The method is validated by using a 1.58 μm distributed feedback(DFB) LD. The absorption spectra of mixture gas of CO_2 and CO are measured by means of the thermal tuning gas sensing system. The center wavelength of each absorption line is compared with the data in HITRAN2012 database. The results show that the deviations are less than 5 pm. This method fully meets the needs of spectroscopic measurement, and can be applied to spectroscopy, optical communications and other fields. 展开更多
关键词 tuning priori spectroscopic validated junction overlapping VCSEL expensive instead gases
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