Open Access
Issue
JNWPU
Volume 38, Number 6, December 2020
Page(s) 1275 - 1283
DOI https://doi.org/10.1051/jnwpu/20203861275
Published online 02 February 2021
  1. Lee S, Brentner K S, Morris P J. Prediction of Acoustic Scattering in the Time Domain Using a Moving Equivalent Source Method[R]. AIAA-2009-3177 [Google Scholar]
  2. Farassat F. Open Rotor Noise Prediction at NASA Langley-Capabilities, Research and Development[R]. NASA TM-2010-216178 [Google Scholar]
  3. Tinetti A F, Dunn M H. Aeroacoustics Noise Prediction Using the Fast Scattering Code[R]. AIAA-2005-3061 [Google Scholar]
  4. Han Zhonghua, Song Wenping, Qiao Zhide. Aeroacoustic Calculation for Helicopter Rotor in Hover and in Forward Flight Based on FW-H Equation[J]. Acta Aeronautic et Astronautic Sinica, 2003, 24 (5): 400– 404 (in Chinese) [Google Scholar]
  5. Zhao Qijun, Xu Gouhua, Wang Shicun. A Numerical Study of High-Speed Impulsive Noise of Helicopter Rotors with the CFD/Kirchhoff Method[J]. Chinese Journal of Computational Physics, 2006, 23 (2): 137– 143 (in Chinese) [Google Scholar]
  6. Cao Yihua, Kang Pengbin, Yu Ziwen. Numerical Simulation of Airfoil-Tip Vortex Interation[J]. Jounral of Aerospace Power, 2003, 18 (3): 604– 607 (in Chinese) [Google Scholar]
  7. Dunn M H, Tinetti A F. Application of Fast Multipole Methods to the NASA Fast Scattering Code[R]. AIAA-2008-2875 [Google Scholar]
  8. Tinetti A F, Dunn M H. Fast Scattering Code(FSC) User's Manual(Version 2.0)[R]. NASA CR-2006-214510 [Google Scholar]
  9. Dunn M H, Tinetti A F. Aeroacoustic Scattering via the Equivalent Source Method[R]. AIAA-2004-2937 [Google Scholar]
  10. Lee S, Erwin J P, Brentner K S. A Method to Predict Acoustic Scattering of Rotorcraft Noise[J]. Journal of the American Helicopter Society, 2009, 54 (4): 1– 15 [Google Scholar]
  11. Lee S, Brentner K S, Morris P J. Time-Domain Approach for Acoustic Scattering of Rotorcraft Noise[C]//American Helicopter Society 64th Annual Forum Proceedings, Texas, 2009 [Google Scholar]
  12. Testa C, Ianniello S, Bernardini G, et al. Sound Scattered by a Helicopter Fuselage in Descent Flight Condition[R]. AIAA-2007-3497 [Google Scholar]
  13. Atalla N, Glegg S. A Ray-Acoustics Approach to Fuselage Scattering of Rotor Noise[R]. AIAA-1990-4013 [Google Scholar]
  14. Fan Feng, Lin Yongfeng, Huang Shuilin, et al. Numercial Simulation on Rotor/Fuselage Unsteady Interaction Flowfield Based on Hybrid Grid[J]. Journal of Naujing University of Aeronautics & Astronautics, 2015, 42 (2): 180– 188 (in Chinese) [Google Scholar]
  15. Roe P L. Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes[J]. Journal of Computational Physics, 1981, 43 (2): 357– 372 [NASA ADS] [CrossRef] [MathSciNet] [Google Scholar]
  16. Jameson A. Time Dependent Calculations Using Multigrid with Application to Unsteady Flows Past Airfoils and Wings[R]. AIAA-1991-1596 [Google Scholar]
  17. Luo H, Baum J D. A Fast Matrix-Free Implicit Method for Computing Low Mach Number Flows on Unstructured Grids[R]. AIAA-1999-3315 [Google Scholar]
  18. Spalart P R, Allmaras S R. An One-Equation Turbulence Model for Aerodynamic Flows[R]. AIAA-1992-0439 [Google Scholar]
  19. DI FRANCESCANTONIO P. A New Boundary Integral Formulation for the Prediction of Sound Radiation[J]. Journal of Sound and Vibration, 1997, 202 (4): 491– 509 [CrossRef] [Google Scholar]
  20. Lee S, Brentner K S, Farassat F, et al. Analytical Formulation and Numerical Implementation of an Acoustic Pressure Gradient Prediction[J]. Journal of Sound and Vibration, 2009, 319 (2009): 1200– 1221 [CrossRef] [Google Scholar]
  21. Boxwell D A, Yu Y H, Schnitz F H. Hovering Impulsive Noise: Some Measured and Calculated Results[R]. NASA CP-2052 [Google Scholar]
  22. Boxwell D A, Schmitz F H, Splettstoesser W R, el al. Model Helicopter Rotor High Speed Impulsive Noise-Measured Acoustics and Blade Pressures[C]//The 9th European Rotorcraft Forum, 1983 [Google Scholar]
  23. Crouse G L, Leishman J G, Bi N. Theoretical and Experimental Study of Unsteady Rotor/Body Aerodynamic Interactions[C]//American Helicopter Society 46th Annual Forum Proceedings, Washington D C, 1990 [Google Scholar]

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