By U.S. Army
This 1972 guide describes the foundations of explosive habit as they practice to liquid and stable explosives, and therefore presents a with ease obtainable choice of very important theoretical and experimental effects on explosives and explosive results. This rfile comprises experiences on: strength of explosives, Thermal decomposition of explosives, dimension of detonation homes, ordinary conception of the airplane detonation wave, software of concept to condensed explosives, constitution of the aircraft detonation wave: finite response quarter, Detonation waves of cylindrical and round symmetry, Thermal explosion, Initiation of detonation by way of surprise waves, Initiation and progress of detonation from effect, friction, and thermal resources, surprise waves from explosive fees, and desktop courses for explosive calculations. This booklet will profit ammunition designers, scientists, and engineers.
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Additional info for Engineering Design Handbook - Principles of Explosive Behavior:
Example text
The general thermodynamic relations are derived for a heterogeneous mixture. First the partial derivatives of volume with respect to temperature and pressure, are derived and then the derivatives of pressure with respect t o volume and temperature are derived. Then specific heats, and derivatives of entropy, energy, enthalpy, and chemical potential are considered. Finally the adiabatic exponent and the sound speeds are derived. The equation of state of a heterogeneous mixture is constructed from the p-u-T relations for each of the constituent phases, making use of the fact that the volume of a mixture is the sum of the volumes of its constituent phases.
2-6 to another form that is due to Riemann. For nondissipative flow as described by the entropy transport equation in the form of Eq. 2-108, the pressure and the sound velocity vary within the flow as functions of the density only. It is then convenient t o introduce the quantity 5 = 0 at Addition and subtraction of the first two of these equations yields the new set [- +(u+c)- "1 ax (u+u)=O I (2-122) [;+u-& =o which is due t o Riemann. The form of Eqs. 2 - 1 2 2 suggests the definition of three characteristic directions-labeled C+, C-, and Co-by the definitions } dx c, : - (2-123) = u dt A characteristic curue in the x,t plane is defined as one that is tangent a t every point to a characteristic direction.
2-29 t o write 6q = Z 6 q f k ) = Tds = cdT h where s is the specific entropy. If the volume is held constant during the heating process, the 2-12 valid either for a change between equilibrium states or for a change at constant composition. It follows that alternate definitions for the heat capacities are given by the expressions cp = (“) aT P 9 cp,n = (g)p,n T o evaluate the frozen heat capacity at constant volume for a heterogeneous system, we introduce the abbreviation (2-58) and employ the identity AMCP 706-180 Expressions for the quantities cr , and (ae/ar),T,n are given in Appendix A, and expressions for the derivatives of the mixture volume are given by Eqs.