Exploring Theoretical Fundamentals of a Physical-Mathematical Model for Unsteady Combustion in Solid Rocket Fuel and Developing Methods for Unsteady Velocity Calculation

Elena Vladimirovna Molchanova Alves, Manuel Joaquim Alves
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Abstract

The article is dedicated to the theoretical study of the non-stationary Combustion Velocity of Solid Rocket Fuel (CVSRF). To calculate the Internal Ballistic Characteristics (IBC) of solid fuel missile engines, combustion velocity laws are used. These laws represent stationary relationships between the Combustion Velocity of Solid Rocket Fuel (CVSRF) and initial pressure and temperature. These relationships are experimentally determined under “stationary” conditions, i.e., by burning fuel samples in stationary conditions.
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探索固体火箭燃料非稳态燃烧物理数学模型的理论基础并开发非稳态速度计算方法
本文致力于固体火箭燃料非稳态燃烧速度(CVSRF)的理论研究。要计算固体燃料导弹发动机的内部弹道特性(IBC),需要使用燃烧速度定律。这些定律代表了固体火箭燃料燃烧速度(CVSRF)与初始压力和温度之间的静态关系。这些关系是在 "静止 "条件下通过实验确定的,即在静止条件下燃烧燃料样品。
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Analytical Solution of Non-Linear Oscillator and Thermal Properties of Interacting System of Real Polyatomic Molecules On the Compactness of Lie Elements On the Convergence of Multi-Stage Differential Transform Method On Self-Adjoint Boundary Value Problems for a Functional Equation of Even Order Exploring Theoretical Fundamentals of a Physical-Mathematical Model for Unsteady Combustion in Solid Rocket Fuel and Developing Methods for Unsteady Velocity Calculation
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