Abstract A numerical model was built for the form function of gun propellant. To simplify the heavy mesh work, the 3D-grain of propellant would be transformed into the porous medium in control volumes. Then, the iterative calculation of solid fraction matrix could be established to reflect the burn-back of burning surface. Finally, based on the weighting sum of matrix element, the percentage of the propellant mass burned (Ψ) varying with the relative propellant thickness (Z) could be obtained as the numerical results for the form function. The step size of Z is dependent on the size of control volume for the geometry simplification, and the accuracy of Ψ-Z relies on the modification factor connecting with the gradient of solid fraction in the iterative process. The present model could adapt to different geometric conditions, such as 7-pore grain and spherical propellant. The deviation magnitude of Ψ would be less than O(10−2).
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