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Laboratory for Mechanisms of Noise Generation and Modal Analysis

Contract number
14.Z50.31.0032
Time span of the project
2014-2018

As of 01.11.2022

10
Number of staff members
52
scientific publications
12
Objects of intellectual property
General information

Name of the project: Development of innovative methods for research of mechanisms of noise generation in turbulent flows

Goals and objectives

Research directions: Aeroacoustics, aviation acoustics, methods of aeroacoustic measurements

Name of the project: Development of innovative methods for research of mechanisms of noise generation in turbulent flows


The practical value of the study

Scientific results:

  • We have developed and tested a method for the azimuthal decomposition of noise from a reactive jet near a hard reflecting surface. For the first time in the world we have conducted measurements of azimuthal modes of noise of an aircraft engine jet on a full-scale test rig.
  • We have developed and tested in laboratory conditions a methodology for measuring the mode composition of noise in the air-intake channel of an air engine.
  • For the first time in the Russian practice we have received experimental data on the azimuthal composition of noise in an air-intake channel and performed a localization of noise sources from a modern aircraft engine.
  • We have developed a methodology for the experimental measurement of acoustic and flight aerodynamic characteristics of moving multipole sources of various sizes on the basis of multichannel measurement methods. A beam forming method has been developed and tested for localizing a dipole-type noise source.

  • We have developed and tested a method for measuring the azimuthal and radial structure of a noise field in a channel in the presence of impedance reflection on the walls. A methodology has been developed for choosing a placement scheme with improved noise cancellation or cells of noise-canceling structures with enhanced noise cancellation in a wide range of frequencies, a method for determining acoustic characteristics of large noise-canceling  structures at a specified azimuthal modal composition of a noise field. 

Implemented results of research:

  • We have created computer software for determining the optimal locations of microphones in flat and ring multmicrophone grids. We processed the measured  acoustic data that allow to determine the modal composition of noise in a channel of an aircraft engine. Two certificates of state registration of software programs have been obtained. These programs were used to refine the testing program  and for processing results of acoustic measurements of an aircraft engine on an open test bench.
  • The laboratory has created computer programs for designing highly-efficient noise-canceling structures (NCS) for channels of aircraft engines. Using this software, we have developed NCS with a resonance cells with new configurations that show better noise cancellation in a wide range of frequencies. Three patents and four certificates of state registration of software programs have been obtained.
  • A technology has been developed for creating NCSs with a higher level of noise cancellation, created prototypes of full-scale NCSs that can be installed onto a prospective Russian aircraft engine, one patent has been obtained.
  • An input device has been developed for a 40-channel rotating mode generator, one patent has been obtained.

  • An interferometer has been developed with controlled contraction of the NCSs sample that allows to reduce the dispersion of the measured acoustic characteristics, one patent has been obtained. 

Education and career development:

  • We have compiled and launched 7 disciplines in the education process of Perm National Research Polytechnic University in the direction of master’s degree training «Aircraft engines»: «Mathematical foundations of acoustics», «Basics of acoustics research», Aeroacoustics», «Modern methods of acoustic measurements», «Theory and practice of acoustic signals and fields processing», «Finite-element methods in problems of acoustics», «Numerical modeling of acoustic processes in aircraft engines».
  • Two additional training programs has been created for professionals from other organizations: 21 professionals have completed training.
  • 14 employees of the Laboratory have enrolled in the postgraduate school.

  • One Doctor of Sciences dissertation, 4 Candidate of Sciences dissertations, 5 specialist s degree theses, 4 master’s degree theses, 5 bachelor’s degree theses have been prepared and defended. 

Organizational and structural changes:

We have created the unique scientific facility  «Acoustically damped chamber with aerodynamic noise sources», it is actively used for conducting research works for grants and commercial agreements. 

Collaborations:
  • Central Aerohydrodynamic Institute – TsAGI (Russia), «UEC–Aviadvigatel» JSC (Russia): joint research, publications, internships of postgraduate and undergraduate students and young researchers.
  • Bruel&Kjaer (Denmark): joint research, creating an optimized antenna for identifying the modal structure of noises in cylindrical channel. 

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BYCHKOV O.P., DEMYANOV M.A., FARANOSOV G.A.
Localization of dipole noise sources using planar microphone arrays Acoustical Physics 65(5): 567-577 (2019).
KOPIEV V.F., KHRAMTSOV I.V., PALCHIKOVSKIY V.V.
Study of the peak frequency in turbulent vortex ring noise Acoustical Physics 65(3): 288-296 (2019).
KOPIEV V.F., KHRAMTSOV I.V., ERSHOV V.V., PALCHIKOVSKIY V.V.
On the possibility of using a single time realization for investigating noise from vortex rings Acoustical Physics 65(1): 67-75 (2019).
FARANOSOV G.A., BELYAEV I.V., KOPIEV V.F., ZAYTSEV M.YU., ALEKSENTSEV A.A., BERSENEV YU.V., CHURSIN V.A., VISKOVA T.A.
Adaptation of the azimuthal decomposition technique to jet noise measurements in full-scale tests. AIAA Journal 55(2): 572 (2017).
FARANOSOV G.A., BYCHKOV O.P.
Two-dimensional model of the interaction of a plane acoustic wave with nozzle edge and wing trailing edge. The Journal of the Acoustical Society of America 141 (1): 289–299 (2017).
KOPIEV V.F., PALCHIKOVSKIY V.V., BELYAEV I.V., BERSENEV YU.V., MAKASHOV S.YU., KHRAMTSOV I.V., KORIN I.A., SOROKIN E.V.
Construction of an anechoic chamber for aeroacoustic experiments and examination of its acoustic parameters. Acoustical Physics 63(1): 113–124 (2017).
OSTRIKOV N.N., SOBOLEV A.F., YAKOVETS M.A., IPATOV M.S., PALCHIKOVSKIY V.V., PAVLOGRADSKIY V.V.
Investigation of impedance eduction accuracy on “interferometer with the flow” test rigs with help of exact solution problem of sound propagation in duct with impedance transition. AIAA Paper 3186 (2017).
GORODKOVA N., CHURSIN V., BERSENEV YU., BURDAKOV R., SINE A., VISKOVA T.
Modal analysis of an aircraft engine fan noise. AIP Conference Proceedings 1770: 030118 (2016).
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