中国科学院力学研究所复现飞行条件高超声速激波风洞JF12的落成突破了毫秒级试验时间的瓶颈,有效试验时间超过100 ms.因此,对于JF12长试验时间激波风洞的测力试验,基于应变天平技术较为成熟、结构简单等优点,我们考虑采用传统的应变计天...中国科学院力学研究所复现飞行条件高超声速激波风洞JF12的落成突破了毫秒级试验时间的瓶颈,有效试验时间超过100 ms.因此,对于JF12长试验时间激波风洞的测力试验,基于应变天平技术较为成熟、结构简单等优点,我们考虑采用传统的应变计天平.但是,激波风洞来流冲击所带来的惯性力干扰导致天平测力系统产生低频振动,传统内置应变天平的结构刚度很难保证信号有足够的处理周期,这大大限制了激波风洞测力模型的尺寸和重量.针对这个难题,基于JF12激波风洞的运行特点及对测力天平刚度特性的特殊要求,优化设计了应变天平的测力单元结构以适用于这种脉冲动态测力试验,相应加工制造了大刚度、低干扰、高灵敏度的系列脉冲型应变天平,结构形式包含了杆式和盒式,最大载荷(法向力)从1 k N到30 k N,以满足不同尺度飞行器的测力试验需求.同时,我们应用不同尺度的测力模型对研制的脉冲型天平在JF12激波风洞进行了一系列动态气动力测量试验,以进一步评估JF12系列脉冲型应变天平的结构特性和测力性能.展开更多
Cellular cell pattern evolution of cylindrically-diverging detonations is numerically simulated successfully by solving two-dimensional Euler equations implemented with an improved two-step chemical kinetic model. Fro...Cellular cell pattern evolution of cylindrically-diverging detonations is numerically simulated successfully by solving two-dimensional Euler equations implemented with an improved two-step chemical kinetic model. From the simulation, three cell bifurcation modes are observed during the evolution and referred to as concave front focusing, kinked and wrinkled wave front instability, and self-merging of cellular cells. Numerical research demonstrates that the wave front expansion resulted from detonation front diverging plays a major role in the cellular cell bifurcation, which can disturb the nonlinearly self-sustained mechanism of detonations and finally lead to cell bifurcations.展开更多
Accurate aerodynamic measurements in the hypersonic flow of large aircraft models in tunnels have practical significance, but pose a significant challenge. Novel aerodynamic force measurement methods have been propose...Accurate aerodynamic measurements in the hypersonic flow of large aircraft models in tunnels have practical significance, but pose a significant challenge. Novel aerodynamic force measurement methods have been proposed,but lack theoretical support. The forms of the force signals techniques for signal processing and calculation of aerodynamics are especially problematic. A theoretical study is conducted to investigate the dynamic properties based on models of the draw-rod system and slender rods. The results indicate that the inertia item can be neglected in the rod governing equation;further, the solutions show that the signals of each rod are a combination of aerodynamic signals（with a constant value） and sine signals, which can be verified by experimental shock tunnel results. Signal processing and aerodynamics calculation techniques are also found to be achievable via the flat part of the signals.展开更多
Cylindrical cellular detonation is numerically investigated by solving two- dimensional reactive Euler equations with a finite volume method on a two-dimensional self-adaptive unstructured mesh. The one-step reversibl...Cylindrical cellular detonation is numerically investigated by solving two- dimensional reactive Euler equations with a finite volume method on a two-dimensional self-adaptive unstructured mesh. The one-step reversible chemical reaction model is applied to simplify the control parameters of chemical reaction. Numerical results demonstrate the evolution of cellular cell splitting of cylindrical cellular detonation explored in experimentas. Split of cellular structures shows different features in the near-field and far-field from the initiation zone. Variation of the local curvature is a key factor in the behavior of cell split of cylindrical cellular detonation in propagation. Numerical results show that split of cellular structures comes from the self-organization of transverse waves corresponding to the development of small disturbances along the detonation front related to detonation instability.展开更多
文摘中国科学院力学研究所复现飞行条件高超声速激波风洞JF12的落成突破了毫秒级试验时间的瓶颈,有效试验时间超过100 ms.因此,对于JF12长试验时间激波风洞的测力试验,基于应变天平技术较为成熟、结构简单等优点,我们考虑采用传统的应变计天平.但是,激波风洞来流冲击所带来的惯性力干扰导致天平测力系统产生低频振动,传统内置应变天平的结构刚度很难保证信号有足够的处理周期,这大大限制了激波风洞测力模型的尺寸和重量.针对这个难题,基于JF12激波风洞的运行特点及对测力天平刚度特性的特殊要求,优化设计了应变天平的测力单元结构以适用于这种脉冲动态测力试验,相应加工制造了大刚度、低干扰、高灵敏度的系列脉冲型应变天平,结构形式包含了杆式和盒式,最大载荷(法向力)从1 k N到30 k N,以满足不同尺度飞行器的测力试验需求.同时,我们应用不同尺度的测力模型对研制的脉冲型天平在JF12激波风洞进行了一系列动态气动力测量试验,以进一步评估JF12系列脉冲型应变天平的结构特性和测力性能.
基金Supported by the National Natural Science Foundation of China under Grant Nos 90205027 and 10632090
文摘Cellular cell pattern evolution of cylindrically-diverging detonations is numerically simulated successfully by solving two-dimensional Euler equations implemented with an improved two-step chemical kinetic model. From the simulation, three cell bifurcation modes are observed during the evolution and referred to as concave front focusing, kinked and wrinkled wave front instability, and self-merging of cellular cells. Numerical research demonstrates that the wave front expansion resulted from detonation front diverging plays a major role in the cellular cell bifurcation, which can disturb the nonlinearly self-sustained mechanism of detonations and finally lead to cell bifurcations.
基金Project supported by the National Natural Science Foundation of China(Grant Nos.11472281 and 11532014)
文摘Accurate aerodynamic measurements in the hypersonic flow of large aircraft models in tunnels have practical significance, but pose a significant challenge. Novel aerodynamic force measurement methods have been proposed,but lack theoretical support. The forms of the force signals techniques for signal processing and calculation of aerodynamics are especially problematic. A theoretical study is conducted to investigate the dynamic properties based on models of the draw-rod system and slender rods. The results indicate that the inertia item can be neglected in the rod governing equation;further, the solutions show that the signals of each rod are a combination of aerodynamic signals（with a constant value） and sine signals, which can be verified by experimental shock tunnel results. Signal processing and aerodynamics calculation techniques are also found to be achievable via the flat part of the signals.
基金the National Natural Science Foundation of China(No.90205027)China Postdoctoral Science Foundation(No.2005037444)
文摘Cylindrical cellular detonation is numerically investigated by solving two- dimensional reactive Euler equations with a finite volume method on a two-dimensional self-adaptive unstructured mesh. The one-step reversible chemical reaction model is applied to simplify the control parameters of chemical reaction. Numerical results demonstrate the evolution of cellular cell splitting of cylindrical cellular detonation explored in experimentas. Split of cellular structures shows different features in the near-field and far-field from the initiation zone. Variation of the local curvature is a key factor in the behavior of cell split of cylindrical cellular detonation in propagation. Numerical results show that split of cellular structures comes from the self-organization of transverse waves corresponding to the development of small disturbances along the detonation front related to detonation instability.
基金the National Key Research and Development Plan of China(Grant No.2019YFA0405204)the National Natural Science Foundation of China(Grant Nos.12172365,12072353,and 12132017).
