Generation of boundary-conforming grids around wing-body configurations using transfinite interpolation

AIAA Journal

Volumn 20, Issue 10, 1982, Pages 1313-1320

  Eriksson, L E ^a  

^a Aeronautical Research Institute of Sweden   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT - WINGS;

GRID GENERATION;

AERODYNAMICS - WINGS AND AIRFOILS;

EID: 17544392187     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.7980     Document Type: Article

References (3)

1. Gordon, W. J. and Hall, C. A., “Construction of Curvilinear Coordinate Systems and Applications of Mesh Generation,” International Journal of Numerical Methods in Engineering, Vol. 7, 1973, pp. 461-477.
2. Eriksson, L. E., “Three-Dimensional Spline-Generated Coordinate Transformations for Grid around Wing-Body Configurations,” Numerical Grid Generation Techniques, NASA CP 2166, 1980.
3. Rizzi, A. W., “Damped Euler-Equation Method to Compute Transonic Flow Around Wing-Body Combinations,” AIAA Journal, 1982, to be published.