Improvements in numerical analysis of droplet impingement using lagrangian approach

SAE Technical Papers

Volumn , Issue , 2011, Pages

  Ke, Peng ^a   Wang, Xinxin ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

DROPS; EFFICIENCY; ENGINES; FIGHTER AIRCRAFT; ITERATIVE METHODS; MASS TRANSFER; SNOW AND ICE REMOVAL;

COMPUTATION METHODS; COMPUTATIONAL RESULTS; DROPLET IMPINGEMENT; HEAT AND MASS TRANSFER; IMPINGEMENT EFFICIENCY; ITERATIVE COMPUTATION; LA-GRANGIAN APPROACHES; LOCALIZATION METHOD;

LAGRANGE MULTIPLIERS;

EID: 85072494974     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/2011-38-0004     Document Type: Conference Paper

References (10)

1. Gent, R.W., Trajice2-a Combined Water Droplet Trajectory and Ice Accretion Prediction Program for Aerofoils [R]. 1990
2. Wright, W.B., Potapczuk, M.G., Levinson, L.H., Comparison of Lewice and Glennice in the Sld Regime [A]. AIAA 2008-0439, 2008
3. Hedde, T., Guffond, D., Onera Three-Dimensional Icing Model [J]. AIAA Journal, 1995, 33 (6), 1038-1045.
4. Morency, F., Tezok, F., Paraschivoiu, I., Anti-Icing System Simulation Using Canice [J]. Journal of Aircraft, 1999, 36 (6), 999-1006.
5. Widhalm, M., Ronzheimer, A., Meyer, J., Lagrangian Particle Tracking on Large Unstructured Three-Dimensional Meshes [A]. AIAA 2008-472, 2008
6. Peng, K., Shuguang, Z., Jianghao, W., et al. An Improved Known Vicinity Algorithm Based on Geometry Test for Particle Localization in Arbitrary Grid [J]. Journal of Computational Physics, 2009.
7. Nathman, J.K., Mccomas, A., Icing Collection Efficiency from Direct Simulation. 2007, 9, 6086-6092.
8. Papadakis, M., Hung, K.E., Vu, G.T., et al. Experimental Investigation of Water Droplet Impingement on Airfoils, Finite Wings, and an S-Duct Engine Inlet [R]. NASA, NASA / TM - 2002-211700, 2002
9. Papadakis, M., Rachman, A., Wong, S.-C., et al. Water Impingement Experiments on a Naca 23012 Airfoil with Simulated Glaze Ice Shapes. 42nd AIAA Aerospace Sciences Meeting and Exhibit, January 5, 2004-January 8, 2004, 2004, 5528-5568.
10. Bidwell, C.S., Mohler, S.R., Collection Efficiency and Ice Accretion Calculations for a Sphere, Aswept Ms(1)-317 Wing, a Swept Naca-0012 Wing Tip, an Axisymmetric Inlet, and a Boeing 737-300 Inlet [A]. AIAA-95-0755, Reno, NV: AIAA, 1995