Ice accretion prediction on multielement airfoils

Journal of Aircraft

Volumn 35, Issue 2, 1998, Pages 240-246

  Mingione, Giuseppe ^a   Brandi, Vincenzo ^a,b  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; HEAT CONVECTION; HEAT TRANSFER COEFFICIENTS; ICE PROBLEMS; THERMODYNAMICS;

ICE ACCRETION PREDICTION; MULTIELEMENT AIRFOILS;

AIRFOILS;

EID: 0032028780     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2290     Document Type: Article

References (20)

1. Hedde, T., and Guffond, D., "Improvement of the ONERA 3-d Icing Code, Comparison with 3D Experimental Shapes," AIAA Paper 93-0169, Jan. 1993.
2. Gent, R. W., "TRAJICE2 - A Combined Water Droplet and Ice Accretion Prediction Code for Airfoils," Royal Aerospace Establishment, TR 90054, May 1990.
3. Wright, W. B., "Users Manual for the Improved NASA Lewis Ice Accretion Code LEWICE 1.6," NASA CR 198355, June 1995.
4. Bidwell, C. S., and Mohler, S. R., "Trajectory and Ice Accretion Calculations for a Swept NACA 0012 Wing, a Swept MS-317 Wing, an Axisymetric Inlet, and a Boeing 737-200 Inlet," AIAA Paper 95-0755, Jan. 1995.
5. Brahimi, M. T., Tran, P., Paraschivoiu, I., and Tezok, F., "Prediction of Ice Accretion on Supercritical and Multi-Element Airfoils," AIAA Paper 95-0754, Jan. 1995.
6. Messinger, B. L., "Equilibrium Temperature of an Unheated Icing Surface as Function of Airspeed," Journal of the Aeronautical Sciences, Vol. 20, No. 1, 1953, pp. 29-42.
7. Olsen, M., and Walker, E., "Experimental Evidence for Modifying the Current Physical Model for the Ice Accretion on Aircraft Surfaces," NASA TM 87184, May 1986.
8. Vicini, A., and Mingione, G., "Computation of Three-Dimensional Droplet Trajectories and Temperature for the C.I.R.A. Icing Wind Tunnel," Italian Aerospace Research Center, CIRA-TN-95-0052, March 1995.
9. Cebeci, T, and Bradshaw, P., Physical and Computational Aspects of Convective Heat Transfer, Springer-Verlag, New York, 1988, pp. 94, 95, 184-201.
10. Kays, W. M., and Crawford, M. E., Convective Heat Transfer, McGraw-Hill, New York, 1980, p. 420.
11. Mingione, G., and Brandi, V., "A Code for the Evaluation of Ice Accretion on Multi-Element Airfoils," Italian Aerospace Research Center, CIRA-TN-96-089, July 1996.
12. Shin, J., and Bond, T., "Results of an Icing Test on a NACA 0012 Airfoil in the NASA Lewis Icing Research Tunnel," AIAA Paper 92-0647, Jan. 1992.
13. Quagliarella, D., "Aerodynamic Analysis of a Flapped Airfoil Configuration for the YAK-130S Airplane," Italian Aerospace Research Center, CIRA-TN-97-038, June 1997.
14. Tran, P., Brahimi, M. T., Tezok, F., and Paraschivoiu, I., "Numerical Simulation of Ice Accretion on Multiple Element Configurations," AIAA Paper 96-0869, Jan. 1996.
15. Wilcox, D. C., "Simulation of Transition with a Two-Equation Turbulence Model," AIAA Journal, Vol. 32, No. 2, 1994, pp. 247-255.
16. Newton, J. E., Van Fossen, G. J., Poinsatte, P. E., and DeWitt, K. J., "Measurement of Local Convective Heat Transfer Coefficients from a Smooth and Roughened NACA 0012 Airfoil: Flight Test Data," AIAA Paper 88-0287, Jan. 1988.
17. Cebeci, T., "The Calculation of Flow over Iced Airfoils," AIAA Paper 88-0112, Jan. 1988.
18. Cooper, W. A., Sand, W. R., Politovich, M. K., and Veal, D. L., "Effects of Icing on Performance of a Research Airplane," Journal of Aircraft, Vol. 21, No. 9, 1984, pp. 708-715.
19. Ashenden, R., and Marwitz, J. D., "Supercooled Large Droplet Distributions in the Natural Environment and Comparison to Artificial Drizzle from Air Force Water Spray-Tanker," Proceedings of the FAA International Conference on Inflight Aircraft Icing (Springfield, VA), DOT/FAA/AR-96/8, II, 1996, pp. 33-43.
20. Heinrich, A., Ross, R., Zumwalt, G., Provorse, J., Padmanabhan, V., Thompson, J., and Riley, J., Aircraft Icing Handbook, Vol. 1, DOT/FAA/CT-88/8-1, March 1991, pp. 1-13.