A high-order immersed boundary method for unsteady incompressible flow calculations

M. N. Linnick, Hermann F Fasel

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

4 Citations (Scopus)

Abstract

Immersed boundary methods are becoming increasingly popular for the computation of unsteady flows around complex geometries using a Cartesian grid. While good results, both qualitative and quantitative, have been obtained, many of the methods rely on low-order corrections to account for the immersed boundary. The objective of the present work is to present a high-order immersed boundary method for the 2-D, unsteady, incompressible Navier-Stokes equations in stream function-vorticity formulation. The method employs an explicit Runge-Kutta (second or fourth order) time integration scheme, fourth-order compact finite-differences for computation of spatial derivatives, and a nine-point, fourth-order compact discretization of the Poisson equation for computation of the stream function. Corrections to the finite-difference stencils are used to maintain high formal accuracy at the immersed boundary, as confirmed by analytical tests. To validate the method in its application to incompressible flows, several physically relevant test cases are computed, including uniform flow past a circular cylinder and Tollmien-Schlichting waves in a boundary layer.

Original languageEnglish (US)
Title of host publication41st Aerospace Sciences Meeting and Exhibit
StatePublished - 2003
Event41st Aerospace Sciences Meeting and Exhibit 2003 - Reno, NV, United States
Duration: Jan 6 2003Jan 9 2003

Other

Other41st Aerospace Sciences Meeting and Exhibit 2003
CountryUnited States
CityReno, NV
Period1/6/031/9/03

Fingerprint

incompressible flow
Incompressible flow
unsteady flow
Poisson equation
Tollmien-Schlichting waves
Unsteady flow
Circular cylinders
Vorticity
uniform flow
Navier Stokes equations
Boundary layers
circular cylinders
Navier-Stokes equation
vorticity
Derivatives
Navier-Stokes equations
boundary layers
Geometry
grids
formulations

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Linnick, M. N., & Fasel, H. F. (2003). A high-order immersed boundary method for unsteady incompressible flow calculations. In 41st Aerospace Sciences Meeting and Exhibit

A high-order immersed boundary method for unsteady incompressible flow calculations. / Linnick, M. N.; Fasel, Hermann F.

41st Aerospace Sciences Meeting and Exhibit. 2003.

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

Linnick, MN & Fasel, HF 2003, A high-order immersed boundary method for unsteady incompressible flow calculations. in 41st Aerospace Sciences Meeting and Exhibit. 41st Aerospace Sciences Meeting and Exhibit 2003, Reno, NV, United States, 1/6/03.
Linnick MN, Fasel HF. A high-order immersed boundary method for unsteady incompressible flow calculations. In 41st Aerospace Sciences Meeting and Exhibit. 2003
Linnick, M. N. ; Fasel, Hermann F. / A high-order immersed boundary method for unsteady incompressible flow calculations. 41st Aerospace Sciences Meeting and Exhibit. 2003.
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