On determining the acoustic properties of main helicopter rotor models on an open test bench


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Abstract

The paper presents the results of experimental studies on developing a technique to determine the acoustic properties of models of main helicopter rotors on an open test bench. The method of maximum length sequences is used to choose the optimum arrangement of microphones for an open test bench that would minimize the influence of parasitic echo. The results of processing the data of an acoustic experiment with a model rotor are detailed.

About the authors

V. F. Kop’ev

Central Aerohydrodynamic Institute; Perm National Research Polytechnical University

Author for correspondence.
Email: aeroacoustics@tsagi.ru
Russian Federation, ul. Radio 17, Moscow, 105005; Komsomol’skii pr. 29, Perm, 614990

M. Yu. Zaitsev

Central Aerohydrodynamic Institute; Perm National Research Polytechnical University

Email: aeroacoustics@tsagi.ru
Russian Federation, ul. Radio 17, Moscow, 105005; Komsomol’skii pr. 29, Perm, 614990

N. N. Ostrikov

Central Aerohydrodynamic Institute; Perm National Research Polytechnical University

Email: aeroacoustics@tsagi.ru
Russian Federation, ul. Radio 17, Moscow, 105005; Komsomol’skii pr. 29, Perm, 614990

S. L. Denisov

Central Aerohydrodynamic Institute

Email: aeroacoustics@tsagi.ru
Russian Federation, ul. Radio 17, Moscow, 105005

S. Yu. Makashov

Central Aerohydrodynamic Institute

Email: aeroacoustics@tsagi.ru
Russian Federation, ul. Radio 17, Moscow, 105005

V. A. Anikin

Kamov Design Bureau

Email: aeroacoustics@tsagi.ru
Russian Federation, Krasnopresnenskaya nab. 12, Moscow, 123610

V. V. Gromov

Kamov Design Bureau

Email: aeroacoustics@tsagi.ru
Russian Federation, Krasnopresnenskaya nab. 12, Moscow, 123610

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