Investigation of the physical processes underlying the ice accretion phenomena

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Tezok, F ^a   Brahimi, M T ^b   Paraschivoiu, I ^b  

^a BOMBARDIER AEROSPACE   (Canada)

^b Aeronautical Chair   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ANGLE OF ATTACK; NASA; THERMOANALYSIS; WINGS;

ACCURACY AND REPEATABILITIES; ANGLES OF ATTACK; ANTI-ICING SYSTEMS; MEASUREMENT METHODS; OBSERVATIONS AND MEASUREMENTS; PHYSICAL PROCESS; PREDICTION CODES; THERMO DYNAMIC ANALYSIS;

ICE;

EID: 85088352278     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-484     Document Type: Conference Paper

References (12)

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3. Hacker, P. T. and Dorsch, R. G., "A summary of Meteorological Conditions Associated with Aircraft Icing and a Proposed Method of Selecting Design Criterions for Ice Protection Equipment," NACA TN 2569, 1951.
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9. Cebeci, T. and Besnard, E., "Progress Towards the Prediction of the Aerodynamic Performance Degradation of an Aircraft in Natural Icing Conditions," Proceedings of the First Bombardier International Workshop on Aircraft Icing and Boundary Layer Stability & Transition, Montreal, Canada, Sept. 20-21, 1993, pp. 56-85.
10. Tezok, F., Fritz, E., "Icing Tunnel Testing Methodology," Proceedings of the 6th Aerodynamics Symposium, CASI, Toronto, Ontario, April 28-30, 1997, pp. 81-100.
11. Brahimi, M. T., Tran, P., and Paraschivoiu, I. "Numerical Simulation and Thermodynamic Analysis of Iće'Accretion on Aircraft Wings," Centre de Developpement Technologique de l'Ecole Polytechnique de Montreal, C. D. T. Project Cl59, Final Report prepared for Canadair, 1994.
12. Messinger, B. L., "Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed," Journal of Aeronautical Sciences, 1953.