Published June 2004 | Version Published
Conference Paper Open

Three-dimensional instabilities of compressible flow over open cavities: direct solution of the BiGlobal eigenvalue problem

  • 1. ROR icon Technical University of Madrid
  • 2. ROR icon California Institute of Technology

Abstract

We report progress in our ongoing effort to compute and understand the instabilities of open cavity flows from incompressible to supersonic speeds. We consider three-dimensional instabilities of nominally two dimensional (spanwise homogeneous) cavity flows (BiGlobal instabilities). Experiments, DNS/LES computations, and preliminary instability computations have shown that the modes of oscillation are influenced by complex interactions between the shear layer and the recirculating flow within the cavity. We present here a framework for computation of the two-dimensional eigenvalue problem for the compressible open cavity. We validate the numerical scheme by computing several canonical flows: square duct flow, boundary layers at speeds from incompressible to supersonic, and two-dimensional parallel shear layers. We present preliminary results for the three-dimensional modes of the compressible open cavity flow with length-to-depth ratio of two at a Mach number of 0.325.

Additional Information

© 2004 by the American Institute of Aeronautics and Astronautics, Inc. Published Online: 19 Jun 2012. The material is based upon work supported by the European Office of Aerospace Research and Development, Air Force Research Laboratory, Air Force Office of Scientific Research, under Grants No. F49620-02-1-0362 (Caltech) and FA8655-03-1-3059 (nu modelling S.L.) monitored by Dr. John D. Schmisseur (AFOSR) and Mr. Wayne Donaldson (EOARD).

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Additional details

Additional titles

Alternative title
Three-Dimensional Instabilities of Compressible Flow over Open Cavities: Direct Solution of hte BiGlobal Eivenvalue Problem

Identifiers

Eprint ID
97265
Resolver ID
CaltechAUTHORS:20190718-165126795

Funding

European Office of Aerospace Research and Development
Air Force Research Laboratory (AFRL)
Air Force Office of Scientific Research (AFOSR)
F49620-02-1-0362
Air Force Office of Scientific Research (AFOSR)
FA8655-03-1-3059

Dates

Created
2019-07-24
Created from EPrint's datestamp field
Updated
2021-11-16
Created from EPrint's last_modified field

Caltech Custom Metadata

Other Numbering System Name
AIAA Paper
Other Numbering System Identifier
2004-2544