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 add
✦ LIBER ✦
Modeling of normal and erosive burning rate of a hot double-base homogeneous propellant
✍ Scribed by Jean-Michel Most; Pierre Joulain; Gérard Lengellé; Jean-Claude Godon
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 622 KB
- Volume
- 105
- Category
- Article
- ISSN
- 0010-2180
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✦ Synopsis
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 transfer between the flame and the wall by the turbulent mechanisms. The calculated burning rate overshoot, generally called erosive burning, accurately predicts the experimentally observed phenomena.
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