A parametric study of the effect of self-oscillating trailing-edge flaplets on aerofoil self-noise

Author:

Talboys Edward,Geyer Thomas F.,Prüfer Florian,Brücker Christoph

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference34 articles.

1. Airfoil self-noise and prediction;Brooks;NASA Ref Publ,1989

2. Paterson RW, Vogt PG, Fink MR, Munch CL. Vortex Noise of Isolated Airfoils, NACA Adv. Restricted Rept. 3G29 J. Aeronaut. Sci. J. Aircr. Low Adv. Ration J. Am. Helicopter Soci-ety J. Aircr. 17; 1972: 3–12.

3. Discrete tones of isolated airfoils;Tam;J Acoust Soc Am,1974

4. Noise generated by airfoil profiles placed in a uniform laminar flow;Arbey;J Fluid Mech,1983

5. Lowson M, Fiddes S, Nash E. Laminar boundary layer aero-acoustic instabilities. In: 32nd Aerosp. Sci. Meet. Exhib. American Institute of Aeronautics and Astronautics: Reston, Virigina; 1994.

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