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Mathematical description of nonstationary aerodynamic characteristics of a passenger aircraft model in longitudinal motion at large angles of attack

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Publication:371359
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DOI10.1134/S0021894411030096zbMath1272.76150OpenAlexW2044544333MaRDI QIDQ371359

V. I. Petoshin, E. A. Chasovnikov

Publication date: 2 October 2013

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

Full work available at URL: https://doi.org/10.1134/s0021894411030096


zbMATH Keywords

mathematical modelharmonic vibrationsaircraft modelfrequency characteristics


Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)


Related Items (2)

Aerodynamic characteristics of a deltawing in the case of harmonic oscillations with respect to the roll and yaw angles at high angles of attack ⋮ Identification of aerodynamic coefficients of longitudinal movement and error estimates for onboard measurements of supercritical angles of attack







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