1. “Influence of Model Parameters and the Vane Response Method on a Low-Order Prediction of Fan Broadband Noise,” Sheryl Grace, International Journal of Aeroacoustics,  January-Marchvol. 151-2: pp. 131143, 2016.
  2. “Fan Broadband Interaction Noise Modeling Using a Low-Order Method,” Sheryl Grace, Journal of Sound and Vibration, 346: 402-423, 2015.,WhmxIE7
  3. “Characteristics of Turbulence in a Turbofan Stage,” Jeremy Maunus, Sheryl Grace, Doug Sondak, and Victor Yakhot, Journal of Turbomachinery, 135(2):021024-1-10 March, 2013..
  4. “Effect of Rotor Wake Structure on Fan Interaction Noise,” Jeremy Maunus, Sheryl Grace, and Doug Sondak, AIAA Journal, 50(4):818-831, Apr., 2012.
  5. “Simulation of the binaural environmental transfer function for gerbils using a boundary element method,” S. M. Grace, E. Quaranta, B. Shinn-Cunningham and H. F. Voigt, Acta Acustica United with Acustica 94:310-320, 2008.
  6. “Experimental Investigation of the Flow Characteristics Within a Shallow Wall Cavity for Both Laminar and Turbulent Upstream Boundary Layers,” S. M. Grace, D. E. Wroblewski, and W. G. Dewar, Experiments in Fluids, 36:791-804, 2004.
  7. “Numerical Simulation of the Forced Wave Equation as an Acoustic Post-processing Technique for CFD,” Sheryl M. Grace, Aerotecnica Missili E Spazio, Journal of the Associazione Italiana di Aeronautica e Astronautica, 79:3-4, 75-80, July-December, 2000.
  8. “Prediction of Low-frequency Tones Produced by Flow Through a Duct with a Gap,” Sheryl M. Grace, Journal of Sound and Vibration, 229(4):859-878, Jan. 2000.
  9. “Inverse Aeroacoustic Problem for a Rectangular Wing in a Gust”, Trevor H. Wood and Sheryl M Grace, AIAA Journal, 38(2):203-210, February, 2000.
  10. “Stability of High Reynolds Number Flow Past a Circular Aperture,” Sheryl M. Grace, Trevor H. Wood, and Michael S. Howe,Proceedings of the Royal Society of London, 455:2055-2066, June, 1999.
  11. “The Influence of Shape on The Rayleigh Conductivity of a Wall Aperture in The Presence of Grazing Flow,” Sheryl M. Grace, Kelly P. Horan and Michael S. Howe, Journal of Fluids and Structures, 12(3):335-351, April, 1998.
  12. “Direct Computations of Unsteady Flows About Thin Airfoils,” Sheryl M. Grace, S. I. Hariharan, and Hafiz M. Atassi, Journal of Computational Acoustics, 6(3):337-355, 1998.
  13. “Modeling the Dynamics of Spring-Driven, Oscillating-Foil Propulsion,” Karen A. Harper, Matthew D. Berkemeier and Sheryl M. Grace, Journal of Oceanic Engineering, 23(3):285-296, July, 1998.
  14. “Inverse Aeroacoustic Problem For A Streamlined Body. Part I: Basic Formulation,” Sheryl M. Patrick Grace, Hafiz M. Atassi and William K. Blake, AIAA Journal, 34(11):2233-2240, November, 1996.
  15. “Inverse Aeroacoustic Problem For A Streamlined Body. Part II: Accuracy of Solutions,” Sheryl M. Patrick Grace, Hafiz M. Atassi and William K. Blake, AIAA Journal, 34(11):2241-2246, November, 1996.
  16. “Direct Calculation of Sound Radiated From Bodies in Nonuniform Flows,” Ha z M. Atassi, Jiseng Fang and Sheryl M. Patrick, Journal of Fluids Engineering, 115:573-579, December 1993.


  1. “Experimental Study of Quadcopter Acoustics and Performance at Static Thrust Conditions,” Nanyaporn Intaratep, W. Nathan Alexander, William Devenport, Sheryl Gracea and Amanda Dropkin, AIAA paper No. 2016-2873, 2016
  2. “Comparison of methods for adding vane geometry in a low-order fan broadband noise prediction.” Sheryl Grace and Dorien Vellafranco, AIAA Paper No. 2016-2946, 2016.
  3. “Further Investigations Into a Low-Order Model of Fan Broadband Noise,” Sheryl Grace, AIAA Paper No. 2015-3283, June 2015.
  4. “Analysis of Mean Loading Effects in Fan Broadband Noise Simulations,” Sheryl M Grace, Tim Farmer, and Lorna Ayton, AIAA Paper, AIAA Paper No. 2014-2944, June, 2014.
  5. “Development of experimental facility for testing human response to ILFN from wind turbines,” Aleks Zosuls, R Kelley, David Mountain, and Sheryl Grace,  POMA 2013-NS1581379-12-18395, ASA, June  2013.
  6. `Prediction of broadband fan exit guide vane response,” Sheryl M Grace and Gilbert Forsyth, AIAA Paper, AIAA Paper No. 2013-2153. June 2013.
  7. “Fan Broadband Interaction Noise Modeling,”  Sheryl Grace, Andy Wixom, Doug Sondak, Michaela Logue, andJulian Winkler, AIAA Paper, AIAA Paper No. 2012-2269. June 2012.
  8. “Wind Turbine Health Impact Study:Report of Independent Expert Panel,”   Jeffrey M. Ellenbogen, Sheryl Grace, Wendy J Heiger-Bernays, James F. Manwell,Dora Anne Mills, Kimberly A. Sullivan, and Marc G. Weisskopf.  January 2012. Web link.
  9. “Effect of CFD Wake Predition in a Hybrid Simulation of Fan Broadband Noise,” Jeremy Maunus, Sheryl Grace, and Doug Sondak, AIAA Paper No. 2011-2875, June 2011.
  10. “Experimental validation of RANS turbulence parameters for turbofans,” Jeremy Maunus, Sheryl Grace, Doug Sondak, and Victor Yakhot. GT2011-45906, ASME Turbo Expo 2011. (presented by Doug Sondak)
  11. “Effect of Rotor Wake Structure on Fan Interaction Noise,” Jeremy Maunus, Sheryl Grace, and Doug Sondak, AIAA Paper No. 2010-3746, 2010. (presented by Jeremy Maunus)
  12. “Hybrid prediction of fan tonal noise,” Sheryl M. Grace, Douglas L. Sondak, Daniel J. Dorney, and Michael Cannamela, AIAA Paper No. 2008-2992, 2008.
  13. “CFD Computation of Fan Interaction Noise,” Sheryl M. Grace, Douglas L. Sondak, Daniel J. Dorney, and Michaela Logue, IMECE2007-43779, Proceedings of the IMECE 07, ASME, Seattle, WA, Nov. 2007.
  14. ASME IMECE Tutorial for NCAD ” Computational Methods for Aeroacoustics
  15. VIE presentations March 2004:  Lectures 1 and 2
  16. Modeling gerbil hearing (presentation) pdf
  17. VKI Presenations march 2001: Lecture 1, Lecture 2, Lecture 3
  18. Editor of “Proceedings of the Noise Control and Acoustics Division 2003”, (IMECE, ASME).
  19. “Wing Geometry Effect on Blade-Vortex Interaction Response Using BEM,” Trevor H. Wood and Sheryl M. Grace, Proceedings of the 2001 ASME IMECE, NCAD, Nov. 2001. presentation
  20. “Unsteady Blade Response: The BVI Model vs. The Gust Model,” Sheryl M. Grace, AIAA Paper No. 2001-2209, 7th AIAA/CEAS Aeroacoustic Conference, Maastricht, The Netherlands, May, 2001.
  21. “An Overview of Computational Aeroacoustic Techniques Applied to Cavity Noise Prediction,” Sheryl M. Grace, AIAA Paper No. 2001-0510, 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2001.
  22. “Time-Dependent Calculation of Acoustic Radiation from Finite Wings Using BEM,” Trevor H. Wood and Sheryl M. Grace, Proceedings for the 2000 ASME IMECE, NCAD, Nov. 2000.
  23. “Implications of Recent BVI Calculations on Prediction Methods for Noise from Turbulence Ingestion,” ASEE Summer Faculty Project Report for NSWC Carderock Division, August, 2000.
  24. “Free-wake Analysis for Calculating The Aeroacoustics of A Wingap Configuration”, Trevor. H.Wood, and Sheryl M. Grace, AIAA Paper No. 2000-0607, 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January, 2000.
  25. “Acoustic Computations Using Incompressible Invscid CFD Results as Input”, Sheryl M. Grace, Caroline K. Curtis, and Allan D. Pierce, Proceedings of the ASME Noise Control and Acoustics Division, ASME IMECE, Nashville, TN, November 1999. (Presented by Allan Pierce).
  26. “Aeroacoustic Predictions of A Wing-Flap Con guration In Three Dimensions,” Trevor H. Wood and Sheryl M. Grace,Paper No. 99-1892, 5th AIAA/CEAS Aeroacoustics Conference, May 10-12, 1999, Seattle WA. (Presented by Trevor Wood)
  27. “Acoustic Energy Absorption by a Shear Layer,” Sheryl M. Grace, AIAA Paper No. 98-2304, 4th AIAA/CEAS Aeroacoustics Conference, June 2-4, 1998, Toulouse, France.
  28. “Inverse Aeroacoustic Problem for a Rectangular Wing in a Gust,” Trevor H. Wood and Sheryl M. Grace, Paper No. 98-2229, 4th AIAA/CEAS Aeroacoustics Conference, June 2-4, 1998, Toulouse, France. (Presented by Trevor Wood).
  29. “Reduction of the Complexity of the Intrinsically Nonlinear Problem of Aerodynamic Sound Generation in an Unbounded Domain,” Sheryl M. Grace and Allan D. Pierce, Proceedings of the IUTAM Symposium on Computational Methods for Unbounded Domains, July, 1997.
  30. “The Influence of Grazing Flow on the Rayleigh Conductivity of an Aperture of Arbitrary Shape,” Sheryl M. Grace, Michael S. Howe, and Kelly P. Horan, Paper No. 97-1672, for the 3rd AIAA/CEAS Aeroacoustics Conference, May, 1997.
  31. “Unsteady Aerodynamic Analysis for a Flat-plate Airfoil in Subsonic Mean Flow,” Sheryl M. Grace, Boston University Tech. Rep. AM-97-004, January, 1997.
  32. “Decreasing the Energy Costs of Swimming Robots through Passive Elastic Elements,” Karen A. Harper, Matthew D. Berkemeier and Sheryl M. Grace,, Proceedings of the 1997 IEEE International Conference on Robotics and Automation. (Presented by Karen Harper).
  33. “Predicting Unsteady Aerodynamic Parameters From Airfoil Surface Pressure Measurements,” Sheryl M. Patrick Grace, NCA-Vol 22, Proceedings of the ASME Noise Control and Acoustics Division, November 1996, pp. 93-98.
  34. “An Inverse Problem in the Presence of a Mean Flow,” Sheryl M. Grace, Boston University Tech. Rep. AM-96-017, August 1996.
  35. “Inverse Aeroacoustic Problem For A Rectangular Wing Interacting With A Gust,” Sheryl M. Patrick and Hafiz M. Atassi, AIAA 96-1790, Presented at 2nd AIAA/CEAS Aeroacoustics Conference, State College, PA, May 1996.
  36. “Predicting The Unsteady Pressure on A Streamlined Body From Its Acoustic Signal,” Sheryl M. Patrick, Hafiz M. Atassi and William K. Blake, CEAS/AIAA-95-162, Proceedings of the CEAS/AIAA Aeroacoustics Conference, Munich, Germany, June 1995, pp.1105-1114.
  37. “The Pressure Field of a Gust Interacting with a Flat Plate,” Sheryl M. Patrick and Hafiz M. Atassi, ICASE/LaRCWorkshop on Benchmark Problems in Computational Aeroacoustics, NASA Conference Publication 3300, May 1995, pp.291-296.
  38. “Inverse Problems in Unsteady Aerodynamics and Aeroacoustics,” Sheryl M. Patrick, Hafiz M. Atassi and William K. Blake, Active Control of Vibration and Noise, ASME DE-Vol. 75, November 1994, pp. 309-319.
  39. “Acoustic Radiation from a Lifting Airfoil in Nonuniform Subsonic Flow,” Sheryl M. Patrick, Hafiz M. Atassi and Catherine M. Davis, Computational Aero- and Hydro Acoustics, ASME FED, 175:117-122, June 1993.