Aeroelastic stability of wing/pylon/rotor coupled system for tiltrotor aircraft in forward flight

DOI10.1007/S11431-011-4454-5zbMath1239.74025OpenAlexW2253738473MaRDI QIDQ425013

ChaoMin Yang, Pin-Qi Xia

Publication date: 7 June 2012

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-011-4454-5

zbMATH Keywords

forward flightelastic couplingaeroelastic stabilitytiltrotor aircraft

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10)

Cites Work

• A wake bending unsteady dynamic inflow model of tiltrotor in conversion flight of tiltrotor aircraft
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