Stabilisation of reduced order models via restarting

Author:

Wales C.1,Gaitonde A.1,Jones D.1

Affiliation:

1. Aerospace Engineering Queen's Building University Walk Bristol; University of Bristol; BS8 1TR; UK

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference31 articles.

1. Computation of unsteady transonic flows by the solution of Euler equations;Venkatakrishnan;AIAA Journal,1988

2. Brenneis A Eberle A Evaluation of an implicit Euler code against two and three-dimensional standard configurations AGARD Conference on Transonic Unsteady Aerodynamics and Aeroelasticity 1992

3. Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations;Guruswamy;AIAA Journal,1990

4. Jameson A Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings 10th Computational Fluid Dynamics Conference, AIAA Paper 91-1596 1991

5. A dual-time method for the solution of the unsteady Euler equations;Gaitonde;Aeronautical Journal,1994

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