基于莫尔层析技术诊断不完全膨胀的三维流场

基于莫尔层析技术，诊断了从不同喷嘴喷出的对称与非对称不完全膨胀气流的密度分布。给出了实验结果，并对该结果分析后，得到几个重要结论，最后，就系统的应用作了展望。     

NUMERICAL SIMULATION OF HIGHLY UNDEREXPANDED AXISYMMETRIC JET WITH RUNGE-KUTTA DISCONTINUOUS GALERKIN FINITE ELEMENT METHOD

Highly undcrexpanded axisymmctric jet was simulated using the Runge-Kutta Discontinuous Galerkin （RKDG） finite element method, which, based on two-dimensional conservation laws, was used to solve the axisymmetric Euler equations. The computed results show that the complicated flow field structures of interest, including shock waves, slipstreams and the triple point observed in experiments could be well captured using the RKDG finite element method. Moreover, comparisons of the Mach disk location exhibit excellent agreements between the computed results and experimental measurements, indicating that this method has high capability of capturing shocks without numerical oscillation and artificial viscosity occurring near the discontinuous point.     

Characteristics of the Mach Disk in the Underexpanded Jet in which the Back Pressure Continuously Changes with Time

When the high-pressure gas is exhausted to the vacuum chamber from the nozzle, the underexpanded supersonic jet contained with the Mach disk is generally formed. The eventual purpose of this study is to clarify the unsteady phenomenon of the underexpanded free jet when the back pressure continuously changes with time. The characteristic of the Mach disk has been clarified in consideration of the diameter and position of it by the numerical analysis in this paper. The sonic jet of the exit Mach number Me=1 is assumed and the axisymmetric conservational equation is solved by the TVD method in the numerical calculation. The diameter and position of the Mach disk differs with the results of a steady jet and the influence on the continuously changing of the back pressure is evidenced from the comparison with the case of steady supersonic jet.     

Transient Flowfield Characteristics of Polycarbonate Plasma Discharge from Pulse-powered Electrothermal Gun Operation

An electrothermal gun is the device that produces high-temperature and high-velocity plasma vapor using high current pulsed power and has a potential to be an efficient method for producing a variety of nanomaterials. Pulsed plasma discharge from the electrothermal gun into the open air has been investigated numerically, and the time-dependent inviscid gas dynamics equations are solved for the two-dimensional computational domain including electrothermal gun and the open-air space using flux-corrected transport (FCT) scheme. The modeling of the Joule heating and the mass ablation from the bore wall are incorporated in the computation. The computational results yield the details of the plasma discharge behavior inside and outside the capillary bore including choked condition at the bore exit and complex shock structure of external plasma discharge. The flow structure of freely expanding plasma discharge in the open air is essentially the highly underexpanded supersonic jet featuring Mach disk, barrel shock, contact surface, and spherical blast wave. Compared to the experiments, the numerical simulation agrees well with the experimental data such as the capillary mass ablation and shock structure of the plasma jet.     

Experimental and Numerical Study of Twin Underexpanded Impinging Jets

In this paper, the dual underexpanded impinging jets are experimentally and numerically studied. The experiments were performed by measuring the unsteady and averaged wall static pressures and by visualizing density fields using schlieren method. Numerical calculations were also conducted by solving unsteady three dimensional compressible Navier-Stokes equations with Baldwin-Lomax turbulence model. The main parameters for the dual jets are the non-dimensional distance between the two nozzle centers HID covering 1.5, 2.0, the nozzle to plate separation LID 2.0, 3.0,4.0 and 5.0 and the pressure ratio defined by po/pb 1.0~6.0, where D is the diameter of each nozzle exit, p0 the stagnation pressure and pb the back pressure. It is found that the agreement between the experiments and the calculations is good. The fountain flow at the middle of the two jets is observed both in the experiments and the calculation. According to FFT analysis of the experiments for the twin jets, relatively low frequency (up to 5     

用莫尔条纹对喷嘴自由喷射的不完全膨胀气流密度的测量

本文应用莫尔条纹法测出了从图形和方形喷嘴里吹出的不完全膨胀气流的密度分布。实验表明，方形喷嘴喷出的气体的密度分布要比圆形喷嘴复杂得多而且在外形上有很大的不同，但沿着两个喷嘴气流轴的气流密度变化非常相似。