首页> 外文会议>International annual conference of ICT >A Complete Equation of State for TNT-Air Mixtures
【24h】

A Complete Equation of State for TNT-Air Mixtures

机译:TNT-空气混合物的完整状态方程

获取原文

摘要

A complete equation of state is proposed for TNT-air mixtures up to 15,000 K. Three components are recognized: (ⅰ) pure TNT, (ⅱ) pure air, and (ⅲ) a mixture of TNT and air; each component is assumed to be in thermodynamic equilibrium. The thermodynamic states were calculated with the Cheetah code. Figure 1 depicts the specific internal E_r(T,R) as a function of temperature T and density ratio R = ρ/ρ_0 . Cheetah has been extended (exp6.v7.0.1.chi library) to include to include ionized species of air an electrons: N+, O+, O-, N2+, N2-, O2+, O2-, NO+, CO+, C+, Ne+, e-; results agree with Gilmore's calculations. This figure illustrates the strong dependence on density at high temperatures. Figure 2 depicts the specific internal energy u(T,R) as a function of T and R for pure TNT. Again one finds a strong dependence on density at high temperatures. Discontinuities in the curves at high density correspond to phase changes. Previous numerical simulations by Brode used an equation of state for TNT as developed by Jones and Miller. Figure 3 presents the specific internal energy E_r(T, R = 1, Y_(air)) as a function of temperature and mass fraction of air: Y_(air) = m_(air)/m_(mixture). At high temperatures there is a monotonic variation in temperature from pure TNT (Y_(air) = 0) to pure air (Y_(air) = 100%) at constant energy. At lower temperatures, there appears a fold in the thermodynamic equilibrium surface (below 1,200 K). The thermodynamic Equation of State (EOS) functions for pure TNT are shown in Figure 4. Illustrated there are the pressure function: p(u,ρ), the sound speed function: a(u,ρ) and the isentropic gamma function: Γ(u,ρ); again jumps come from phase changes. In our Godunov code, the algorithm requires pressure, sound speed and gamma in each cell, which are computed from these aforementioned EOS functions. Figure 5 presents the specific internal energy u(T, ρ) of pure TNT in the low temperature regime. Also shown there is the CJ isentrope which was used to define the u-T relationship for TNT in previous studies; it illustrates the complexity introduced by density variations in TNT over the range: 0.001 ≤ ρ(g / cc) ≤ 2.16.
机译:对于不超过15,000 K的TNT-空气混合物,提出了一个完整的状态方程。认识到三个成分:(ⅰ)纯TNT,(ⅱ)纯空气,和(ⅲ)TNT和空气的混合物;假定每个组分都处于热力学平衡状态。用猎豹代码计算热力学状态。图1描绘了特定的内部E_r(T,R)与温度T和密度比R =ρ/ρ_0的关系。猎豹已扩展(exp6.v7.0.1.chi库)以包括空气中的离子化物种,包括电子:N +,O +,O-,N2 +,N2-,O2 +,O2-,NO +,CO +,C +,Ne +, e-;结果与Gilmore的计算结果一致。该图说明了高温下对密度的强烈依赖性。图2描绘了纯TNT的比内能u(T,R)与T和R的关系。再次发现在高温下强烈依赖密度。高密度曲线的不连续性对应于相位变化。 Brode先前的数值模拟使用了Jones和Miller开发的TNT的状态方程。图3给出了特定的内部能量E_r(T,R = 1,Y_(空气))与温度和空气质量分数的关系:Y_(空气)= m_(空气)/ m_(混合物)。在高温下,在恒定能量下,温度从纯TNT(Y_(空气)= 0)到纯空气(Y_(空气)= 100%)存在单调变化。在较低的温度下,热力学平衡表面会出现褶皱(低于1200 K)。纯TNT的热力学状态方程(EOS)函数如图4所示。图中显示了压力函数:p(u,ρ),声速函数:a(u,ρ)和等熵伽马函数:Γ (u,ρ);相位变化再次导致跳跃。在我们的Godunov代码中,该算法需要每个单元中的压力,声速和伽马,这些是根据上述EOS函数计算得出的。图5给出了低温条件下纯TNT的比内能u(T,ρ)。还显示了在以前的研究中用于定义TNT的u-T关系的CJ异构体;它说明了在0.001≤ρ(g / cc)≤2.16范围内TNT的密度变化所带来的复杂性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利