Measuring the Acoustic Characteristics of a Helicopter Rotormodel in a Wind Tunnel

Author:

Pakhov V. V.,Fayzullin K. V.,Denisov S. L.

Publisher

Pleiades Publishing Ltd

Subject

Acoustics and Ultrasonics

Reference8 articles.

1. D. A. Boxwell, F. H. Schmitz, W. R. Splettstoesser, and K. J. Schultz, Helicopter Model Rotor-Blade Vortex Interaction Impulsive Noise: Scalability and Parametric Variations, NASATM-86007, A-9854, NAS 1.15:86007, TM-84-A-7, AD-A159471.

2. V. F. Kop’ev, M. Yu. Zaitsev, N. N. Ostrikov, S. L. Denisov, S. Yu. Makashov, V. A. Anikin, and V. V. Gromov, Acoust. Phys. 62, 741 (2016).

3. D. A. Boxwell, F. H. Schmitz, W. R. Splettstoesser, and K. J. Schultz, J. Am. Helicopter Soc. 32 (1), 3 (1987).

4. F. H. Schmitz, E. Greenwood, R. D. Sickenberger, G. Gopalan, B.W.-C. Sim, D. A. Conner, E. Moralez, and W. Decker, in Proc. American Helicopter Society 63rd Annual Forum (Virginia Beach, VA, 2007).

5. R. Stepanov, V. Pakhov, A. Bozhenko, A. Batrakov, L. Garipova, A. Kusyumov, S. Mikhaylov, and G. Barakos, Int. J. Aeroacoust. 16, 460 (2017).

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