EQUATION FOR CALCULATING THE BURNING RATE FOR SOLID PROPELLANTS

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DOI10.17654/AM100020153zbMath1428.74012OpenAlexW2898412773WikidataQ129046792 ScholiaQ129046792MaRDI QIDQ5208911

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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/am100020153

zbMATH Keywords

solid propellant rocket engine burning rate physico-mathematical model condensed phase inside ballistic characteristics

Mathematics Subject Classification ID

Thermodynamics in solid mechanics (74A15) Combustion (80A25)

Related Items (1)

LINEARIZED INTEGRAL EQUATION FOR BURNING RATE OF SOLID PROPELLANTS

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