Optimization of global kinetics parameters for heterogeneous propellant combustion using a genetic algorithm

DOI10.1080/13647830601028949zbMath1117.80306OpenAlexW2024303887MaRDI QIDQ5758180

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Publication date: 3 September 2007

Published in: Combustion Theory and Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/13647830601028949

zbMATH Keywords

optimizationcombustionpropellantsAP/HTPBglobal-kineticsHMX/HTPB

Mathematics Subject Classification ID

Approximation methods and heuristics in mathematical programming (90C59) Combustion (80A25) Chemically reacting flows (80A32) Optimization problems in thermodynamics and heat transfer (80M50) Chemical kinetics in thermodynamics and heat transfer (80A30)

Cites Work

• Computationally efficient, numerically exact design space derivatives via the complex Taylor's series expansion method
• Application of continuation techniques to ammonium perchlorate plane flames

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