3D solutions of the Euler equations on the adaptive tetrahedral meshes

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 22, Issue 6, 2001, Pages 495-499

  Wang, Ping ^a   Zhu, Zi Qiang ^a   Tuo, Shuang Fen ^a   Yin, Xing Yu ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Adaptive grid technique; Euler equation; Unstructured grid; Upwind scheme

Indexed keywords

ADAPTIVE ALGORITHMS; SUPERSONIC FLOW; THREE DIMENSIONAL; TRANSONIC FLOW;

ADAPTIVE GRID ALGORITHM; EULER EQUATION; UNSTRUCTURED GRID; UPWIND SCHEME;

AERODYNAMICS;

EID: 0035521648     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (14)

1. Flux splitting scheme
2. +
3. Generation of three-dimensional unstructured-grids by the advancing-front method
4. Direct surface triangulation using the advancing front method
5. Unstructured meshes and surface fidelity for complex shapes
6. Structured background grids for generation of unstructured grids by advancing-front method
7. Upwind scheme for solving the Euler equations on unstructured tetrahedral meshes
8. Fast upwind solver for the Euler equations on three-dimensional unstructured meshes
9. Pressure distributions on the ONERA M6-Wing at transonic Mach number
10. Supersonic aerodynamic characteristics of a Sparrow III type missile model with wing controls and comparison with existing tail-control results