Model for Development of Backlash in Aircraft Control Circuit Mechanical Links

A model was developed to identify the effect of limit cycle oscillations (LCOs) on wear characteristics of a wing-aileron system in incompressible flow. The wear in the wing-aileron system with freeplay was shown to be a coupled problem.

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Bibliographische Detailangaben
Veröffentlicht in:	Journal of aircraft 1999-03, Vol.36 (2), p.480-482
Hauptverfasser:	Safi, S. A, Kelly, D. W, Archer, R. D
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Mathematical models Physics Solid mechanics Structural and continuum mechanics Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...) Vibrations and mechanical waves
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Beschreibung
Zusammenfassung:	A model was developed to identify the effect of limit cycle oscillations (LCOs) on wear characteristics of a wing-aileron system in incompressible flow. The wear in the wing-aileron system with freeplay was shown to be a coupled problem.
ISSN:	0021-8669 1533-3868
DOI:	10.2514/2.2459