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A modification of the composite propellant erosive burning model of lenoir and robillard

✍ Scribed by Merrill K. King

Publisher
Elsevier Science
Year
1975
Tongue
English
Weight
232 KB
Volume
24
Category
Article
ISSN
0010-2180

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✦ Synopsis

The Lenoir and Robillard model for the erosive burning of composite propellants is shown to suffer from use of an incorrect additivity law for coupling of the effects of heat feedback from the propellant flame and feedback from the core gas. A revised expression, employing a physically realistic additivity concept is derived and shown to fit data from an independent source at least as well as the original expression.

πŸ“œ SIMILAR VOLUMES

Modeling of normal and erosive burning r
Modeling of normal and erosive burning rate of a hot double-base homogeneous propellant
✍ Jean-Michel Most; Pierre Joulain; GΓ©rard LengellΓ©; Jean-Claude Godon πŸ“‚ Article πŸ“… 1996 πŸ› Elsevier Science 🌐 English βš– 622 KB

The burning rate of a hot double-base homogeneous solid propellant is modeled by the numerical solution of the conservation equations characterizing the primary flame using a global kinetic scheme. The increase of the burning rate above the solid surface is modeled by an enhancement of the heat tran