A CARTESIAN CUT CELL METHOD FOR COMPRESSIBLE FLOWS .B. MOVING BODY PROBLEMS

Citation
G. Yang et al., A CARTESIAN CUT CELL METHOD FOR COMPRESSIBLE FLOWS .B. MOVING BODY PROBLEMS, Aeronautical Journal, 101(1002), 1997, pp. 57-65
Citations number
13
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00019240
Volume
101
Issue
1002
Year of publication
1997
Pages
57 - 65
Database
ISI
SICI code
0001-9240(1997)101:1002<57:ACCCMF>2.0.ZU;2-T
Abstract
A cartesian cut cell method for static body problems was presented in part A (pp 47-56). Here, we extend the method to unsteady compressible flows involving arbitrarily moving bodies. The moving bodies are allo wed to cross a stationary background cartesian mesh. So problems such as mesh distortion and/or restrictions on body motion which may affect other mesh approaches do not occur. A MUSCL-Hancock finite volume sch eme has been modified for moving boundary problems. The upwind fluxes on the interfaces of static cells are updated using an HLLC approximat e Riemann solver and an exact Riemann solution for a moving piston is used to update moving solid boundaries (faces). A cell merging techniq ue has been developed to maintain numerical stability in the presence of arbitrarily small cut cells and to retain strict conservation at mo ving boundaries. The method has been validated against some well-known two dimensional test problems and applied to practical examples invol ving an exploding pressure vessel and a store release into a Mach 1 . 5 stream.