Calculation of flight vehicle main support wheel vibrations taking into account brake forces

A model of the main support of the aircraft landing gear is presented and its dynamics is studied using the equations for the distributed motion of a wheel equipped with a brake. Stability of the support wheel rolling motion is analyzed and the brake parameter values which may cause stability loss a...

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Veröffentlicht in:	Russian aeronautics 2012-04, Vol.55 (2), p.144-150
Hauptverfasser:	Metrikin, V. S., Peisel’, M. A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Automotive Engineering Automotive wheels Brakes Dynamic tests Engineering Mathematical analysis Mathematical models Rolling motion Stability Structural Mechanics and Strength of Flight Vehicles Vibration
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Beschreibung
Zusammenfassung:	A model of the main support of the aircraft landing gear is presented and its dynamics is studied using the equations for the distributed motion of a wheel equipped with a brake. Stability of the support wheel rolling motion is analyzed and the brake parameter values which may cause stability loss are found. The results of numerical experiments are presented.
ISSN:	1068-7998 1934-7901
DOI:	10.3103/S1068799812020055