Influence of the Ignition Transient on the Mechanical Response ofComposite Solid Propellants
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Abstract:
Based on an effective nonlinear viscoelastic model, the differential constitutive equation and strain-rate equation of solid composite propellants are induced.Pressure/strain and pressurization rate/strain rate are linear correlation during the ignition transient.And the coefficient is the initial modulus of composite solid propellants.
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ZHONG Tao, ZHANG Weihua, WANG Zhongwei. Influence of the Ignition Transient on the Mechanical Response ofComposite Solid Propellants[J]. Journal of National University of Defense Technology,2004,26(3):7-10.