Evaluation of three turbulence models in static air loads and dynamic stall predictions

Journal of Aircraft

Volumn 27, Issue 4, 1990, Pages 382-384

  Wu, Jiunn Chi ^a   Huff, Dennis L ^b   Sankar, L N ^c,d  

^a NATIONAL CENTRAL UNIVERSITY   (Taiwan)

^b NASA GLENN RESEARCH CENTER   (United States)

^c GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^d School of Aerospace Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTERS--APPLICATIONS; FLOW OF FLUIDS--TURBULENT; FLUID MECHANICS; MATHEMATICAL MODELS;

BALDWIN-LOMAX MODEL; DYNAMIC STALL PREDICTIONS; STATIC AIR LOADS; STEADY FLOW STUDIES; THREE TURBULENCE MODELS; TURBULENCE MODELS;

AERODYNAMICS;

EID: 0025415694     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.25285     Document Type: Article

References (9)

1. Wu, J.-C., "A Study of Unsteady Turbulent Flow Past Airfoils," Ph.D. Thesis, Georgia Institute of Technology, Atlanta, GA, June 1988.
2. Wu, J.-C., Huff, D., and Sankar, L. N., "Evaluation of Three Turbulence Models for the Prediction of Steady and Unsteady Airloads," AIAA Paper 89-0609, Jan. 1989.
3. Steger, J. L., "Implicit Finite Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries," AIAA Journal, Vol. 18, No. 7, 1978, pp. 679-686.
4. Jameson, A., Schmidt, W., and Turkel, E., "Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time Stepping Schemes," AIAA Paper 81-1259, 1981.
5. Baldwin, B. S. and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78- 0257, Jan. 1978.
6. Johnson, D. A. and King, L. S., "A Mathematically Simple Turbulence Closure Model for Attached and Separated Turbulent Boundary Layers," AIAA Journal, Vol. 23, No. 11, Nov. 1985, pp. 1684-1692.
7. Gorski, J. J., "A New Near-Wall Formulation for the k-e Equations of Turbulence," AIAA Paper 86-0556, 1986.
8. McAlister, K. W., Pucci, S. L., McCroskey, W. L., and Carr, L. W., "An Experimental Study of Dynamic Stall in Advanced Airfoil Sections, Vol. 2, Pressure and Force Data," NASA TM 84245, Sept. 1982.
9. Harris, C. D., "Two-Dimensional Aerodynamic Characteristics of the NACA 0012 Airfoil in the Langley 8-foot Transonic Pressure Tunnel," NASA TM-81927, 1981.