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FENSAP-ICE Applications to Complete Rotorcraft Configurations
Technical Paper
2003-01-2105
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The FENSAP-ICE system was first conceived for fixed-wing aircraft and air induction system icing, but major developments are underway to augment its capabilities for icing simulation of rotorcraft and tiltrotor aircraft. A project is underway, under the auspices of the RITA (Rotorcraft Industry Technology Association) to reduce icing certification flight tests through use of second-generation three-dimensional (3D) Computational Fluid Dynamics (CFD) based technologies. The plan is to supplement traditional icing tunnel and flight-testing with modern 3D inflight icing simulation tools that facilitate the development and certification of all-weather operations rotorcraft and tilt-rotor aircraft. A viscous fully 3D ice accretion and runback modeling capability is being developed and initial correlation studies to both 2D and 3D icing test cases have produced very good results. An actuator disk model has also been developed to account for the effects of the main and tail rotors on the flow field and the subsequent changes to ice accretion patterns. The present paper will describe droplet impingement and ice accretion results in terms of increasing geometrical complexity from 2D trimmed airfoil sections, to full 3D tiltrotor aircraft in forward flight, with propellers modeled.
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Tran, P., Baruzzi, G., Akel, I., Habashi, W. et al., "FENSAP-ICE Applications to Complete Rotorcraft Configurations," SAE Technical Paper 2003-01-2105, 2003, https://doi.org/10.4271/2003-01-2105.Also In
References
- Habashi, W.G. “Putting Computers on Ice,” ICAO Journal 50 7 October 1995 14 17
- Baruzzi, G.S. Habashi, W.G. Guèvremont, G. Hafez, M.M. “A Second Order Finite Element Method for the Solution of the Transonic Euler and Navier-Stokes Equations,” International Journal of Numerical Methods in Fluids 20 671 693 1995
- Dompierre, J. Cronin, D. Bourgault, Y. Baruzzi, G. Habashi, W.G. “Numerical Simulation of Performance Degradation of Ice Contaminated Airfoils,” AIAA Paper 97-2235, 15th AIAA Applied Aerodynamics Conference Atlanta June 1997
- Bourgault, Y. Habashi, W.G. Dompierre, J. Baruzzi, G.S. “A Finite Element Method Study of Eulerian Droplets Impingement Models,” International Journal of Numerical Methods in Fluids 29 429 449 1999
- Bourgault, Y. Beaugendre, H. Habashi, W.G. “Development of a Shallow Water Icing Model in FENSAP-ICE,” AIAA Journal of Aircraft 37 640 646 2000
- Beaugendre H. Morency F. Habashi W.G. “ICE3D, FENSAP-ICE's 3D Inflight Ice Accretion Module,” AIAA Journal of Aircraft February 2002
- Croce, G. Habashi, W.G. “Thermal Analysis of Wing Anti-Icing Devices” “Computational Analysis of Convection Heat Transfer,” Comini G. Sundén B. Wessex Institute of Technology Press 2000 409 432
- Bidwell, C.S. Potapczuk, M.G. “Users Manual for the NASA Lewis Three-Dimensional Ice Accretion Code (LEWICE3D),” December 1993
- Von Mises R. “Theory of Flight,” Dover Publications New York 1959
- Chaffin M.S. “A guide to the Use of the Pressure Disk Rotor model as Implemented in INS3D-UP,” September 1995
- Croce, G. Beaugendre, H. Habashi, W.G. “CHT3D: FENSAP-ICE Conjugate Heat Transfer Computations with Droplet Impingement and Runback Effects,” AIAA Paper 2002-0386, 40 th Aerospace Sciences Meeting & Exhibit Reno January 2002
- Habashi, W.G. Dompierre, J. Bourgault, Y. Fortin, M. Vallet, M.-G. “Certifiable Computational Fluid Dynamics Through Mesh Optimization,” AIAA Journal 36 1998 5 703 711
- Morency, F. Beaugendre, H. Baruzzi, G.S. “FENSAP-ICE: A Comprehensive 3D Simulation Tool for Inflight Icing,” AIAA Paper 2001-2566, 15 th AIAA Computational Fluid Dynamics Conference Anaheim, CA June 2001
- Beaugendre, H. Morency, F. Habashi, W.G. “ICE3D, FENSAP-ICE's 3D Inflight Ice Accretion Module,” AIAA Paper 2002-7134, 40 th Aerospace Sciences Meeting & Exhibit Reno January 2002
- Lepage C.Y. Suerich-Gulick F. Habashi W.G. “Anisotropic 3D Mesh Adaptation on Unstructured Hybrid Meshes,” AIAA Paper 2002-0859, 40th AIAA Aerospace Sciences Meeting Reno January 2002