MATHEMATICAL MODEL AND CALCULATION OF THE UNSTEADY COMBUSTION RATE OF THE METALLIZED SOLID ROCKET PROPELLANTS
Author:
Publisher
Tomsk State University
Subject
Mechanical Engineering,Mechanics of Materials,General Mathematics,Computational Mechanics
Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Simulation of the Nonstationary Burning of a Solid Propellant in a Combustion Chamber and Calculation of the Acoustic Admittance of the Combustion Surface of this Propellant;Journal of Engineering Physics and Thermophysics;2023-05
2. Mathematical Modelling on Extinction of Metallized Composite Solid Propellant Under a Sudden Drop in Pressure;Propellants, Explosives, Pyrotechnics;2021-08-16
3. MATHEMATICAL MODELING OF THE METALLIZED SOLID PROPELLANT IGNITION BY A HIGH-TEMPERATURE CONVECTIVE FLOW;Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mekhanika;2020
4. Numerical simulation of the unsteady combustion of solid rocket propellants at a harmonic pressure change;Journal of Mechanical Science and Technology;2020-01
5. Mathematical combustion model of nanoaluminum-air suspension;Combustion Theory and Modelling;2019-09-22
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