LINEARIZED INTEGRAL EQUATION FOR BURNING RATE OF SOLID PROPELLANTS

DOI10.17654/AM100030217zbMath1428.74014OpenAlexW2903704744WikidataQ128710155 ScholiaQ128710155MaRDI QIDQ5208915

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Publication date: 22 January 2020

Published in: Far East Journal of Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.17654/am100030217

zbMATH Keywords

chemical reactionrocket enginephysico-mathematical modelcondensed phasesolid propellantsgas dynamicinside ballistic characteristicsburning speed

Mathematics Subject Classification ID

Thermodynamics in solid mechanics (74A15) Gas dynamics (general theory) (76N15) Combustion (80A25) Chemical kinetics in thermodynamics and heat transfer (80A30)

Cites Work

• A Simplified Model of Unstable Burning in Solid Propellants
• EQUATION FOR CALCULATING THE BURNING RATE FOR SOLID PROPELLANTS
• FUNDAMENTAL SOLUTION OF HEAT EQUATION IN CONDENSED PHASE

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