Open Access
Issue
MATEC Web Conf.
Volume 114, 2017
2017 International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2017)
Article Number 03003
Number of page(s) 7
Section Chapter 3: Aerospace
DOI https://doi.org/10.1051/matecconf/201711403003
Published online 10 July 2017
  1. R.A. Kroeger, H.D. Gruschka, T.C. Helvey, Air Force Flight Dynamics Laboratory Technical Report Low speed aerodynamics for ultra-quiet flight., 71-75 (1971). [Google Scholar]
  2. G.M. Lilley, A study of the silent flight of the owl. AIAA Paper, 98-2340 (1998). [Google Scholar]
  3. G.M. Lilley, The Prediction of Airframe Noise and Comparison with Experiment. Journal of Sound and Vibration, 239(4), 849–859 (2001). [CrossRef] [Google Scholar]
  4. D.P. Lockard, G.M. Lilley, The Airframe Noise Reduction Chanllenge. NASA/TM-2004-213013 (2004). [Google Scholar]
  5. R.R. Graham, The silent flight of owls. J. R. Aeronaut., 38, 837–843 (1934). [CrossRef] [Google Scholar]
  6. M.S. Howe, Aerodynamic noise of a serrated trailing edge. J. Fluids and Structures, 5, 33–45 (1991). [CrossRef] [Google Scholar]
  7. M.S. Howe, On the added mass of a perforated shell, with application to the generation of aerodynamic sound by a perforated trailing edge. Proc. R. Soc. Lond. A, 365, 209–233 (1979). [CrossRef] [Google Scholar]
  8. S. Oerlemans, M. Fisher, T. Maeder, K. Kogler, Reduction of wind turbine noise using optimized airfoils and trailing edge serrations. AIAA J., 47(6):1470–1481 (2009). [CrossRef] [Google Scholar]
  9. M. Herr, New Results in Numerical and Experimental Fluid Mechanics V: Experimental Study on Noise Reduction through Trailing Edge Brushes, Springer, Berlin Heidelberg, 365–372 (2006). [Google Scholar]
  10. M. Herr, W. Dobrzynski, Experimental investigations in low-noise trailing-edge design. AIAA J., 43(6), 1167–1175 (2005). [CrossRef] [Google Scholar]
  11. M. Herr, On the design of silent trailing edges. New Res. in Num. and Exp. Fluid Mech. VI, NNFM 96, 96, 430–437 (2007). [CrossRef] [Google Scholar]
  12. T. Geyer, E. Sarradj, C. Fritzsche, Porous airfoils: Noise reduction and boundary layer effects. AIAA Paper, 2009-3392 (2009). [Google Scholar]
  13. T. Geyer, E. Sarradj, C. Fritzsche, Measurement of the noise generation at the trailing edge of porous airfoils. Exp. in Fluids, 48, 291–308 (2010). [CrossRef] [Google Scholar]
  14. T.S. Liu, K. Kuykendoll, R. Rhew, S. Jones, Avian wing geometry and kinematics, AIAA J., 44, 954–963 (2006). [CrossRef] [Google Scholar]
  15. S. Klan, T. Bachmann, M. Klaas, H. Wagner, W. Schroder, Experimental analysis of the flow field over a novel owl based airfoil. Exp. in Fluids, 46, 975–989 (2009). [CrossRef] [Google Scholar]
  16. R.A. Kroeger, H.D. Gruschka, T.C. Helvey, Low speed aerodynamics for ultra-quiet flight. Air Force Flight Dynamics Laboratory Technical Report, 71-75 (1971). [Google Scholar]
  17. C. Ge, Z. Zhang, P. Liang, C. Zhang, L. Ren, Prediction and control of trailing edge noise based on bionic airfoil. SCIENCE CHINA Technological Sciences E, 57(7), 1462–1470 (2014). [CrossRef] [Google Scholar]
  18. Burgmann, S., Dannemann, J., Schroder W. Time-resolved and volumetric PIV measurements of a transitional separation bubble on an SD7003 airfoil. Exp. in Fluids, 44(4), 609–622 (2008). [CrossRef] [Google Scholar]

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