Modern Research Topics in Aerospace Propulsion 1991
DOI: 10.1007/978-1-4612-0945-4_7
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Combustion Modeling and Stability of Double-Base Solid Rocket Propellants

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Cited by 5 publications
(2 citation statements)
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“…In general, the solution of Eqs. (3)(4)(5)(6)(7)(8) requires numerical methods for both unsteady [q(t)] and steady (q = const) conditions. However, an approximate steady-state analytical solution exists for the case of the large activation energy, EJRT -> oo.…”
Section: Distributed Reaction Modelmentioning
confidence: 99%
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“…In general, the solution of Eqs. (3)(4)(5)(6)(7)(8) requires numerical methods for both unsteady [q(t)] and steady (q = const) conditions. However, an approximate steady-state analytical solution exists for the case of the large activation energy, EJRT -> oo.…”
Section: Distributed Reaction Modelmentioning
confidence: 99%
“…The surface reaction (QSC) model and (30)] and the distributed reaction (non-QSC) model [Eqs. (3)(4)(5)(6)(7)(8)] were both solved numerically using explicit fourth-order compact differencing.…”
Section: Surface Reaction Modelmentioning
confidence: 99%