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A Complete Equation of State for TNT-Air Mixtures

机译:TNT-AIR混合物的完整方程

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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:为TNT - 空气混合物提出了一种完整的状态方程,其高达15,000k。识别出三种组分:(Ⅰ)纯TNT,(Ⅱ)纯空气,(Ⅲ)TNT和空气的混合物;假设每个组件处于热力学平衡。使用猎豹代码计算热力学状态。图1描绘了作为温度T和密度比R =ρ/ρ_0的函数的特定内部E_R(T,R)。猎豹已经扩展(EXP6.V7.0.1.CHI图书馆),包括包括电离的空气物种电子:N +,O +,O-,N2 +,N2-,O2 +,O2-,NO +,CO +,C +,NE +, E-;结果同意Gilmore的计算。该图说明了在高温下密度的强依赖性。图2描绘了作为纯TNT的T和R的功能的特定内部能量U(T,R)。人们再次发现高温密度的强烈依赖。高密度下曲线中的不连续性对应于相变。前面的数字模拟通过琼斯和米勒开发的TNT的状态方程使用。图3显示了特定的内部能量E_R(T,R = 1,Y_(空气))作为空气的温度和质量分数的函数:Y_(空气)= M_(空气)/ m_(混合物)。在高温下,在恒定能量下,从纯TNT(Y_(空气)= 0)到纯空气(Y_(空气)= 100%)的温度的单调变化。在较低的温度下,热力学平衡表面(低于1,200k)时出现折叠。纯TNT的状态(EOS)功能的热力学方程如图4所示。所示,有压力功能:P(U,ρ),声速功能:A(U,ρ)和等式伽马功能:γ (U,ρ);再次跳跃来自相变。在我们的Godunov代码中,该算法在每个单元中需要压力,声速和伽马,从这些上述EOS功能计算。图5显示了低温制度中纯TNT的特定内部能量U(T,ρ)。还示出了CJ Isentrope,用于定义先前研究中TNT的U-T关系;它说明了TNT在范围内的密度变化引入的复杂性:0.001≤ρ(g / cc)≤2.16。

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