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Rotating KirchhofF Method for Three-Dimensional Transonic Blade- Vortex Interaction Hover Noise
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Washington, DC, May
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Lyrintzis, A. S., Kilaras, M. S., and Xue, Y., “Transonic 3-D BVI Noise Using a Rotating KirchhofF Formulation for Advancing Rotors,” 50th AHS Annual Forum, Washington, DC, May 1994.
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3
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A Computational Study of the Aeroacoustics of Rotors in Hover
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49Th AHS Annual Forum
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Baeder, J.D.1
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4
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0029345448
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Unstructured Adaptive Mesh Computations of Rotorcraft High-Speed Impulsive Noise
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Computation of Helicopter Rotor Noise in Forward Flight
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Strawn, R.C.1
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Rotor Aeroacoustics at High-Speed Forward Flight using a Coupled Full Potential/Kirchhoff Method
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St. Petersburg, Russia, Aug
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Polacsek, C., and Costes, M., “Rotor Aeroacoustics at High-Speed Forward Flight using a Coupled Full Potential/Kirchhoff Method,” 21st European Rotorcraft Forum, St. Petersburg, Russia, Aug. 1995.
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21St European Rotorcraft Forum
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Polacsek, C.1
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10
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Kirchhoff Acoustic Methodology Validation and Implementation in the Tiltrotor Aeroacoustic Codes (TRAC)
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Bridgeport, CT, Oct
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Lyrintzis, A. S., Koutsavdis, E. K., Berizin, C. R., Visintainer, J. A., and Pollack, M. J., “Kirchhoff Acoustic Methodology Validation and Implementation in the Tiltrotor Aeroacoustic Codes (TRAC),” 2nd AHS Aeromechanics Specialists’ Conference, Bridgeport, CT, Oct. 1995.
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Lyrintzis, A.S.1
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Pollack, M.J.5
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11
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Duque, E. P. N., Strawn, R. C., Ahmad, J., and Biswas, R., “An Overset Grid Navier- Stokes/Kirchhoff-Surface Method for Rotorcraft Aeroacoustic Predictions,” 34th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 1996, Paper 96- 0152.
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34Th AIAA Aerospace Sciences Meeting
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Duque, E.P.N.1
Strawn, R.C.2
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12
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St. Petersburg, Russia, Aug
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Lowson, M., “Directionality of Helicopter BVI Noise,” 21st European Rotorcraft Forum, St. Petersburg, Russia, Aug. 1995.
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13
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84977107508
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Blade- Vortex Interaction Directivity Studies Using Trace Mach Number
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Bridgeport, CT, Oct
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Sun, B. W-C., George, A. R., and Yen, S. J., “Blade- Vortex Interaction Directivity Studies Using Trace Mach Number,” 2nd AHS Aeromechanics Specialists' Conference, Bridgeport, CT, Oct. 1995.
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Sun, B.W.1
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14
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Flowfield of a Lifting Rotor in Hover: A Navier-Stokes Simulation
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Srinivasan, G. R., Baeder, J. D., Obayashi, S., and McCroskey, W. J., “Flowfield of a Lifting Rotor in Hover: A Navier-Stokes Simulation,” AIAA Journal, Vol. 30, No. 10, Oct. 1992, pp. 2371-2378.
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15
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TURNS: A Free-Wake Euler/Navier-Stokes Numerical Method for Helicopter Rotors
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Extension of Kirchhoff’s Formula to Radiation from Moving Surfaces
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19
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Model-Rotor High- Speed Impulsive Noise: Full-Scale Comparisons and Parametric Variations
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Schmitz, F. H., Boxwell, D. A., Splettstoesser, W. R., and Schultz, K. J., “Model-Rotor High- Speed Impulsive Noise: Full-Scale Comparisons and Parametric Variations,” Vertica, Vol 8, No. 4, 1984, pp. 395-422.
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A Study of Blade-Vortex Interaction Aeroacoustics Utilizing an Independently-Generated Vortex
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Kitaplioglu, C., and Caradonna, F. X., “A Study of Blade-Vortex Interaction Aeroacoustics Utilizing an Independently-Generated Vortex,” AGARD Fluid Dynamics Panel Symposium on Aerodynamics and Aeroacoustics of Rotorcraft, Berlin, Germany, Oct. 1994.
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Computational Aeroacoustic Study of Blade-Vortex Interaction Noise
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Baeder, J. D., and Srinivasan, G. R., “Computational Aeroacoustic Study of Blade-Vortex Interaction Noise,” AHS Aeromechanics Specialists’ Meeting, San Francisco, CA, Jan. 1994.
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An Experimental and Computational Study of Rotor-Vortex Interactions
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Euler Calculations of Unsteady Interaction of Advancing Rotor with a Line Vortex
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Srinivasan, G. R., and McCroskey, W. J., “Euler Calculations of Unsteady Interaction of Advancing Rotor with a Line Vortex,” AIAA Journal, Vol. 31, No. 9, Sep. 1993.
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