Space-time discontinuous Galerkin finite element method for inviscid gas dynamics

Computational Fluid and Solid Mechanics 2003

Volumn , Issue , 2003, Pages 1181-1184

  Van der Ven, H ^a   van der Vegt, J J W ^b   Bouwman, E G ^b  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^b UNIVERSITY OF TWENTE   (Netherlands)

Author keywords

Discontinuous Galerkin finite element methods; Dynamic grid motion; Fluid structure interaction; Gas dynamics

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DYNAMICS; FLUID STRUCTURE INTERACTION; GALERKIN METHODS; GAS DYNAMICS;

DISCONTINUOUS GALERKIN FINITE-ELEMENT METHOD; DOMAIN BOUNDARY; DYNAMIC GRID; EQUATIONS OF GAS DYNAMICS; INVISCID GAS; MOVING MESH; SPACE TIME;

FINITE ELEMENT METHOD;

EID: 33748420169     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-008044046-0.50289-X     Document Type: Chapter

References (5)

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3. Van der Vegt JJW, Van der Ven H Space-time discontinuous Galerkin finite element method with dynamic grid motion for inviscid compressible flows. I. General formulation. J Comput Phys 2002, 182:546-585.
4. Van der Ven H, Van der Vegt JJW Space-time discontinuous Galerkin finite element method with dynamic grid motion for inviscid compressible flows. II. Efficient flux quadrature. Comput Meth Appl Mech Engrg 2002, 191:4747-4780.
5. Yates EC, Land NS, Fougher JT Measured and calculated subsonic and transonic flutter characteristics of a 45° swept-back wing planform in air and freon-12 in the Langley transonic dynamics tunnel. NASA TN D1616 1989.