Numerical Simulation of Rotor-Fuselage Aerodynamic Interaction Using an Unstructured Overset Mesh Technique |
Lee, Bum-Seok
(Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology)
Jung, Mun-Seung (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) Kwon, Oh-Joon (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) Kang, Hee-Jung (Rotorcraft Department, Rotorcraft Development Division, Korea Aerospace Research Institute) |
1 | E. M. Raymond and S. A. Gorton, "Steady and Periodic Pressure Measurements on a Generic Helicopter Fuselage Model in the Presence of a Rotor", NASA TM 2000-210286, 2000. |
2 | A. R. Kenyon and R. E. Brown., “Wake Dynamics and Rotor Fuselage Aerodynamic Interactions”, Presented at the AHS 63rd Annual Forum, Virginia Beach, May 1-3, 2007. |
3 | W. G. Bousman, “Aerodynamic Characteristics of SC1095 and SC 1094 R8 Airfoils”, NASA/TP-2003-212265, 2003. |
4 | K. B. Hilbert, “A Mathematical Model of the UH-60 Helicopter”, NASA TM 85890, 1984. |
5 | B. E. Wake and J. D. Beader, “Evaluation of a Navier-Stokes Analysis Method for Hover Performance Prediction”, Journal of the American Helicopter Society, Vol. 41, No. 1, pp. 7-17, 1996. DOI |
6 | Y. M. Park, H. J. Nam, and O. J. Kwon, “Simulation of Unsteady Rotor-Fuselage Interactions Using Unstructured Adaptive Meshes”, Journal of the American Helicopter Society, Vol. 51, No. 2, pp. 141-149, 2006. DOI |
7 | N. S. Hariharan, and L. N. Sankar, “Numerical Simulation of the Fuselage-Rotor Interaction Phenomenon”, AIAA Paper 96-0672, 1996. |
8 | R. Stangl, and S. Wagner, “Euler Simulation of a Helicopter Configuration in Forward Flight using a Chimera Technique”, Proceedings of the 52nd Annual Forum of the American Helicopter Society, pp. 453-462, 1996. |
9 | M. Dindar, A. Z. Lemnios, M. S. Shephard, and J. E. Flaherty, “An Adaptive Solution Procedure for Rotorcraft Aerodynamics”, AIAA Paper 98-2417, 1998. |
10 | H. J. Kang, and O. J. Kwon, “Effect of Wake Adaptation on Rotor Hover Simulations Using Unstructured Meshes”, Journal of the Aircraft, Vol. 38, No. 5, pp. 868-877, 2001. DOI ScienceOn |
11 | H. J. Kang, and O. J. Kwon, “Unstructured Mesh Navier-Stokes Calculations of the Flowfield of a Helicopter Rotor in Hover”, Journal of the American Helicopter Society, Vol. 47, No. 2, pp. 90-99, 2002. DOI |
12 | P. L. Roe, “Approximate Riemann Solvers, Parameter Vectors and Difference”, Journal of Computational Physics, Vol.43, No. 2, pp. 357-372, 1981. DOI ScienceOn |
13 | M. S. Jung and O. J. Kwon, “A Parallel Unstructured Hybrid Overset Mesh Technique for Unsteady Viscous Flow Simulations”, Presented at the International conference on Parallel Computational Fluid Dynamics, ParCFD 2007-024, 2007. |
14 | M. S. Jung and O. J. Kwon, “A Conservative Overset Mesh Scheme via Intergrid Boundary Reconnection on Unstructured Meshes”, AIAA Paper 2009-3536, San Antonio, TX, June 2009. |
15 | D. A. Wachspress, T. R. Quackenbush, and A.H. Boschitsch, “Rotorcraft Interactional Aerodynamics with Fast Vortex/Fast Panel Methods”, Journal of the American Helicopter Society, Vol. 48, No. 4, October 2003. DOI |
16 | K. Nakahashi, F. Togashi, and D. Sharov, “Intergrid-Boundary Definition Method for Overset Unstructured Grid Approach”, AIAA Journal, Vol. 38, No. 11, pp. 2077-2084, 2000. DOI ScienceOn |
17 | D. N. Marvris, N. M. Kmerath, and H. M.McMahon, “Prediction of Aerodynamic Rotor-Airframe Interactions in Forward Flight”, Journal of the American Helicopter Society, Vol. 34, No. 4, pp. 37-46, 1989. DOI |
18 | P. E. Lorber, and T.A. Egolf, “An Unsteady Helicopter Rotor-Fuselage Aerodynamic Interaction Analysis”, Journal of the American Helicopter Society, Vol. 35, No. 3, pp. 32-42, 1990. DOI |
19 | M. S. Chaffin, and J. D . Berry, “Helicopter Fuselage Aerodynamics Under a Rotor by Navier-Stokes Simulation”, Journal of the American Helicopter Society, Vol. 42, No. 3, pp.235-243, 1997. DOI |
20 | D. D. Boyd, and R. W. Barnwell, “A Computational Model for Rotor-Fuselage Interactional Aerodynamics”, AIAA Paper 2000-0256, AIAA 38th Aerospace Sciences Meeting & Exhibit, Reno NV, January 10-13, 2000. |