Numerical investigation of the unsteady behavior of supersonic plane wakes

P. J. Harris, Hermann F Fasel

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Scopus citations

Abstract

The flow in the wake region of a two-dimensional body has been studied using direct numerical simulations. The nature of instabilities in the wake and its bounding shear layers is addressed for a Mach number of M = 2.46, and the structures that arise from these instabilities are observed. A code was developed to solve the compressible Navier- Stokes equations in two or three dimensions. A spatial model is used, with the computational domain arranged around the trailing edge of a two-dimensional flat plate with a blunt base. Starting at Reynolds numbers of about Re = 30,000, the flow becomes two-dimensionally unstable with respect to sinuous disturbances, resulting in the periodic formation of vorticity structures. Starting at about Re = 100,000, an intermittent shear layer instability was also found, excited by sinuous disturbances. The two instability modes interact to produce a “chaotic” behavior. Above Re = 200,000, the shear layer instability appears without the presence of the sinuous disturbances, forming rows of vortices in the shear layers. Preliminary three-dimensional simulations were carried out, examining the variation in the growth rate of three-dimensional disturbances with spanwise wavelength.

Original languageEnglish (US)
Title of host publication29th AIAA Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages1-11
Number of pages11
ISBN (Print)9780000000002
DOIs
StatePublished - 1998
Event29th AIAA Fluid Dynamics Conference - Albuquerque, United States
Duration: Jun 15 1998Jun 18 1998

Other

Other29th AIAA Fluid Dynamics Conference
CountryUnited States
CityAlbuquerque
Period6/15/986/18/98

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ASJC Scopus subject areas

  • Engineering (miscellaneous)
  • Aerospace Engineering

Cite this

Harris, P. J., & Fasel, H. F. (1998). Numerical investigation of the unsteady behavior of supersonic plane wakes. In 29th AIAA Fluid Dynamics Conference (pp. 1-11). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.1998-2974