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On Multidimensional Global Eigenvalue Problems for Hydrodynamic and Aeroacoustic instabilities

Theofilis, Vassilios (2009) On Multidimensional Global Eigenvalue Problems for Hydrodynamic and Aeroacoustic instabilities. In: 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 05/01/2009 - 08/01/2009, Orlando, Florida, USA.

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Item Type:Presentation at Congress or Day (Article)
Authors/Creators:
Creators NameCreators email (if known)
Theofilis, Vassilios
Title:On Multidimensional Global Eigenvalue Problems for Hydrodynamic and Aeroacoustic instabilities
Event Title:47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
Event Dates:05/01/2009 - 08/01/2009
Event Location:Orlando, Florida, USA
Title of Book:2009 AIAA Meeting Papers on Disc. Conference Proceeding Series
Publisher:American Institute of Aeronautics and Astronautics, AIAA
Date:2009
ISBN:978-1-56347-969-4
Volume:14, Issue 1
Department:Motopropulsión and thermofluidynamic
Faculty:E.T.S.I. Aeronautical (UPM)
Creative Commons licenses:Recognition - No derivative works - No commercial
Item ID:5692
Subjects:Mechanics
Aeronautics

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Official URL: http://www.aiaa.org/content.cfm?pageid=534&id=1781

Abstract

The present effort discusses multi-dimensional eigenvalue problems as applied to the solution of hydro- dynamic and aeroacoustic instability problems on complex geometries. As a demonstrator, global linear instability analyses of steady lamina flows on an elliptic cone in compressible ¿¿ows are monitored; one such flow, obtained using a standard aerodynamics solver, is presented figure 1. Flows on this geometry are intrinsically three-dimensional; as a matter of fact the three-dimensionality of the geometry of the elliptic cone accounts for the departure of the laminar-turbulent transition process from the fairly well-understood scenarios on circular cones and other axisymmetric bodies of revolution. Shedding light on the essentially three-dimensional transition process on the elliptic cone provides motivation for several recent experimental and numerical efforts, as well as for the theoretical/numerical methodology described herein.

Item Type:Presentation at Congress or Day (Article)
Subjects:Mechanics
Aeronautics
Código ID:5692
Depositado Por:Memoria Investigacion
Depositado el:13 Jan 2011 11:26
Last Modified:13 Jan 2011 11:26

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