Mechanical phenomena in ground run of an aircraft with near-critical slip angles
Authors: Plakhtienko, N.; Shifrin, B.
Source: International Applied Mechanics, Volume 42, Number 6, June 2006 , pp. 714-720(7)
Abstract:The paper is concerned with mechanical phenomena accompanying ground run of aircraft with near-critical slip angles. Such phenomena (reduced effectiveness of directional control, self-excited frictional vibrations of a landing gear, internal resonance of an aileron, transverse oscillations of the legs of a multileg landing gear) are due to the nonlinear dependence of the side force on the slip angles
Keywords: aileron; directional control; internal resonance; mechanical phenomena; multileg landing gear; nonlinear dependence; self-excited frictional oscillations; side force; slip angle; transverse vibrations
Document Type: Research Article
Publication date: 2006-06-01