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Application of FENSAP-ICE-Unsteady to Helicopter Icing
Technical Paper
2007-01-3310
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The applicability of FENSAP-ICE-Unsteady to solve ice accretion on rotating helicopter blades is investigated using a two-bladed rotor and a generic cylinder, to represent a fuselage, for a forward flight test case. The unsteady rime ice accretion is simulated by coupling, at each time step, flow and water drop equations to the Messinger icing model. Mesh displacement effects are taken into account by an Arbitrary Lagrangian-Eulerian method. This new icing model is applied to rotor/fuselage flows by considering two grid domains: the first being fixed around the fuselage, and the second rotating with the blades. The gap region is stitched with tetrahedral elements to fully guarantee flow conservation.
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Aubé, M., Baruzzi, G., Habashi, W., and Aliaga, C., "Application of FENSAP-ICE-Unsteady to Helicopter Icing," SAE Technical Paper 2007-01-3310, 2007, https://doi.org/10.4271/2007-01-3310.Also In
References
- Baruzzi G. Tran P. Habashi W.G. Narramore J.C. “Actuator Disk Implementation in FENSAP-ICE, a 3D Navier-Stokes In-Flight Icing Simulation System,” AIAA Paper 2003-0619 2003
- Benoit C. Jeanfaivre G. “3D Inviscid Rotor and Fuselage Calculations Using Chimera and Automatic Cartesian Partitioning Methods,” Journal of the AHS 48 2 April 2003
- Pomin H. Wagner S. “Aeroelastic Analysis of Helicopter Rotor Blades on Deformable Chimera Grids,” Journal of Aircraft 41 3 May-June 2004
- Park Y.M. Nam H.J. Kwon O.J. “Simulation of Unsteady Rotor-Fuselage Interactions Using Unstructured Adaptive Meshes,” American Helicopter Society 59 th Annual Forum Phoenix, Arizona May 6-9 2003
- Benoit C. Jeanfaivre G. Canonne E. “Synthesis of ONERA Chimera Method Developed in the Frame of CHANCE Program,” 31 st European Rotorcraft Forum Firenze, Italy September 13-15 2005
- Hsu J.M. Jameson A. “An Implicit-Explicit Hybrid Scheme for Calculating Complex Unsteady Flows,” AIAA Paper 2002-0714 2002
- Habashi W.G. Morency F. Beaugendre H. “FENSAP-ICE: A Second Generation 3D CFD-based In-Flight Icing Simulation System,” SAE Paper 2003-01-2157 2003
- Beaugendre H. Morency F. Habashi W.G. “FENSAP-ICE: Roughness Effects on Ice Shape Prediction,” AIAA Paper 2003-1222 2003
- Yasushi I. Shih A.M. Soni B.K. “Reliable Isotropic Tetrahedral Mesh Generation Based on an Advancing Front Method,” Proceedings of the 13 th Int. Meshing Roundtable Williamsburg, VA, Sandia September 19-22 2004
- Field D.A. “Automatic generation of transitional meshes,” International Journal for Numerical Methods in Engineering 50 8 March 2001
- Liou S.G. Komerath N.M. McMahon H.M. “Velocity Measurements of Airframe Effects on a Rotor in Low-Speed Forward Flight,” Journal of Aircraft 26 4 April 1989
- Liou, S.G. Komerath, N.M. McMahon, H.M. “Measurement of the Interaction Between a Rotor Tip Vortex and a Cylinder,” AIAA Journal 28 6 June 1990
- Liou S.G. Komerath N.M. McMahon H.M. “Velocity Field of a Cylinder in the Wake of a Rotor in Forward Flight,” Journal of Aircraft 27 9 September 1990
- Mavris D.N. Komerath N.M. McMahon H.M. “Prediction of Aerodynamic Rotor-Airframe Interactions in Forward Flight,” Journal of the American Helicopter Society October 1989