Unsteady processes in aerospace power units with stage separation

DOI10.1016/0021-8928(95)00130-1zbMath0923.76071OpenAlexW2023861097MaRDI QIDQ1370039

S. A. Egorushkin, F. A. Slobodkina

Publication date: 4 November 1997

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(95)00130-1

zbMATH Keywords

combustion chamberbooster bodychange in ramjet ductcritical cross-section of jetdynamic loads on wallsflame stabilizerspropulsion burnout

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Combustion (80A25) Reaction effects in flows (76V05)

Cites Work

• Unsteady gas dynamic processes in ramjets
• Monotonic scheme of the second order of approximation for the continuous calculation of non-equilibrium flows

This page was built for publication: Unsteady processes in aerospace power units with stage separation