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Information Journal Paper

Title

(ENG. NOTE) NUMERICAL SIMULATION OF SOLID ROCKET MOTOR INTERNAL BALLISTICS, USING DYNAMIC MESH

Pages

  1-10

Abstract

 Internal ballistics of SOLID ROCKET MOTOR is simulated by solving the axisymmetric Navier-Stokes equations on a moving unstructured grid. Then, the flow velocity, pressure, temperature, and other variables are computed for problems with complex geometries and boundary conditions. The dynamic (moving) mesh is used to model flows where the shape of the domain changes with time due to motion of the domain boundaries (burning surfaces).Updating of the mesh is handled automatically at each time step, based on the new position of the boundaries. This study showed that CFD with unstructured dynamic meshing can be a powerful tool for simulating internal ballistics of SOLID ROCKET MOTORs.

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    APA: Copy

    HEIDARI, M.R., & RAZZAGHI, B.. (2010). (ENG. NOTE) NUMERICAL SIMULATION OF SOLID ROCKET MOTOR INTERNAL BALLISTICS, USING DYNAMIC MESH. AEROSPACE MECHANICS JOURNAL, 6(2 (20)), 1-10. SID. https://sid.ir/paper/101998/en

    Vancouver: Copy

    HEIDARI M.R., RAZZAGHI B.. (ENG. NOTE) NUMERICAL SIMULATION OF SOLID ROCKET MOTOR INTERNAL BALLISTICS, USING DYNAMIC MESH. AEROSPACE MECHANICS JOURNAL[Internet]. 2010;6(2 (20)):1-10. Available from: https://sid.ir/paper/101998/en

    IEEE: Copy

    M.R. HEIDARI, and B. RAZZAGHI, “(ENG. NOTE) NUMERICAL SIMULATION OF SOLID ROCKET MOTOR INTERNAL BALLISTICS, USING DYNAMIC MESH,” AEROSPACE MECHANICS JOURNAL, vol. 6, no. 2 (20), pp. 1–10, 2010, [Online]. Available: https://sid.ir/paper/101998/en

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