Observatorio de I+D+i UPM

Descripción
The computation of the friction saturated vibratory response of an aerodynamically unstable bladed­disk in a realistic config­ uration is a formidable numerical task, even for the simplified case of assuming the aerodynamic forces to be linear. The non­ linear friction forces effectively couple different traveling waves modes and, in order to properly capture the dynamics of the sys­ tem, large time simulations are typically required to reach a fi­ nal, saturated state. Despite of all the above complications, the output of the system (in the friction microslip regime) is not that complex: it typically consists of a superposition of the aeroelas­ tic unstable traveling waves (TW), which oscillate at the elastic modal frequency and exhibit also a modulation in a much longer time scale. This large time modulation over the purely elastic os­ cillation is due to both, the small aerodynamic effects and the small nonlinear friction forces. The correct computation of these two small effects (small as compared with the elastic forces) is crucial to determine the final amplitude of the flutter vibration, which basically results from its balance. In this work we ap­ ply asymptotic techniques to obtain a simplified model that gives only the slow time dynamics of the amplitudes of the travel­ ing waves, filtering out the fast elastic oscillation. We analyze the stability of the resulting nonlinear TW solutions, and we also compare quantitatively the results of the simplified model with those from a more detailed model that is much more expensive to compute.
Internacional	Si
Nombre congreso	ASME Turbo Expo 2014
Tipo de participación	960
Lugar del congreso
Revisores	Si
ISBN o ISSN	978-0-7918-4567-7
DOI
Fecha inicio congreso	16/06/2014
Fecha fin congreso	20/06/2014
Desde la página	1
Hasta la página	11
Título de las actas	2014 Proceedings of the Asme Turbo Expo 2014

Esta actividad pertenece a memorias de investigación

• Autor: Carlos Martel Escobar (UPM)
• Autor: Rahul Ivaturi . (UPM)
• Autor: Roque Corral Garcia (UPM)

• Creador: Grupo de Investigación: Dinámica y estabilidad no lineal en ingeniería aeroespacial
• Departamento: Matemática Aplicada a la Ingeniería Aeroespacial
• Departamento: Mecánica de Fluidos y Propulsión Aeroespacial