Computing aerodynamic performance of 2D iced airfoils: Blocking strategy and convergence rate

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Zhu, B ^a   Chi, X ^a   Shih, T I P ^a   Slater, J W ^b  

^a Michigan State University   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; ICE; SHEAR FLOW; SHEAR STRESS; TURBULENCE MODELS;

AERO-DYNAMIC PERFORMANCE; ANGLES OF ATTACK; COMPRESSIBLE NAVIER-STOKES EQUATIONS; CONVERGENCE RATES; ENSEMBLE-AVERAGED; MULTI-BLOCK GRID; SHEAR-STRESS TRANSPORT; UNSTRUCTURED GRID;

NAVIER STOKES EQUATIONS;

EID: 85067316901     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-3049     Document Type: Conference Paper

References (6)

1. Addy, H.E., "Ice Accretions and Icing Effects for Modern Airfoils," NASA/TP-2000-210031, April 2000.
2. Chi, X., Zhu, B., Shih, T.I-P., Slater, J.W., Addy, H.E., and Choo, Y.K., "Computing Aerodynamic Performance of 2D Iced Airfoils: Blocking Topology and Grid Generation," AIAA Paper 2002-0381, January 2002.
3. Power, G.D. and Underwood, M.L., "WIND 2.0: Progress on an Applications-Oriented CFD Code," AIAA Paper 99-3212, June 1999.
4. Michal, T. and Oser, M., "Improving Zonal Coupling Accuracy and Robustness in the WIND Code," AIAA Paper 2001-0222, Jan. 2001.
5. Tai, T.C., "Single-Block Structured Body-Conforming Grid for Complex Geometries," Numerical Grid Generation in Computational Field Simulations, edited by B.K. Soni, J.F. Thompson, J. Hauser, and P. R. Eiseman, ISGG, Mississippi State University, 2000, pp. 91-100.
6. Chung, J.J. and Addy, H.E., "A Numerical Evaluation of Icing Effects on a Natural Laminar Flow Airfoil," AIAA Paper 2000-0096, Jan. 2000.