Aircraft performance obtained from modified point mass model

DOI10.1002/ZAMM.20010811589zbMATH Open1014.70020OpenAlexW2082735684MaRDI QIDQ2746089

S. Janković, M. Vrdoljak

Publication date: 7 July 2003

Published in: ZAMM. Zeitschrift für Angewandte Mathematik und Mechanik (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/zamm.20010811589

zbMATH Keywords

variable massfuel consumptiongravity centermodified point mass modelrigid aircraftsteady straight flightsustained turn

Mathematics Subject Classification ID

Free motion of a rigid body (70E15) Variable mass, rockets (70P05)

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