31st Thermophysics Conference 1996
DOI: 10.2514/6.1996-1811
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A coupled thermo-ablative and fluid dynamic analysis for numerical application to solid propellant rockets

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Cited by 4 publications
(4 citation statements)
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“…The ablation process is simplified following the assumption used by Baiocco and Bellomi [11], namely the injection velocity (also called Stephan velocity) is assumed to be orthogonal to the receding surface (tangential components are set to zero). Hence, this new boundary condition prescribes the boundary values for the conservation equations (of mass, momentum, species and energy) to mimic the behavior of an ablated isothermal wall.…”
Section: Boundary Condition For Surface Ablationmentioning
confidence: 99%
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“…The ablation process is simplified following the assumption used by Baiocco and Bellomi [11], namely the injection velocity (also called Stephan velocity) is assumed to be orthogonal to the receding surface (tangential components are set to zero). Hence, this new boundary condition prescribes the boundary values for the conservation equations (of mass, momentum, species and energy) to mimic the behavior of an ablated isothermal wall.…”
Section: Boundary Condition For Surface Ablationmentioning
confidence: 99%
“…The Hirschfleder and Curtiss approximation with correction velocity, equations (9,11,12), are then used to evaluate the normal diffusion flux of each species at the ablated wall:…”
Section: Boundary Condition For Surface Ablationmentioning
confidence: 99%
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“…Many studies have already proposed to couple numerically the gaseous phase and the solid structure [3,4,5]. However, most of them are dedicated to the structural material characterization by predicting the recession rate or the surface temperature and few are dealing with the fluid characterization.…”
Section: Introductionmentioning
confidence: 99%