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The possibility of reducing the noise produced in an airplane cabin by the turbulent boundary layer by varying the fuselage stiffening set with its mass being invariant.
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- Acoustical Physics, 2015, v. 61, n. 5, p. 580, doi. 10.1134/S1063771015040041
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Evaluation of the effect of stopping selected frames on noise in the cabin of a propeller airplane.
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- Acoustical Physics, 2015, v. 61, n. 4, p. 466, doi. 10.1134/S106377101504003X
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- Article
Distinctive features of the pressure fluctuation fields in the vicinities of bulges.
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- Fluid Dynamics, 2015, v. 50, n. 1, p. 50, doi. 10.1134/S0015462815010068
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- Article
Evaluating the Efficiency of Protective Grids on Pressure Pulse Sensors During Aerodynamic Interactions.
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- Measurement Techniques, 2015, v. 57, n. 10, p. 1197, doi. 10.1007/s11018-015-0602-9
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- Article
Calculation of bulkhead vibrations in a supported shell simulating a plane fuselage.
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- Acoustical Physics, 2014, v. 60, n. 5, p. 562, doi. 10.1134/S1063771014040046
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- Article
A complex of analytical models for predicting noise in an aircraft cabin.
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- Acoustical Physics, 2012, v. 58, n. 4, p. 404, doi. 10.1134/S1063771012040057
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- Article
A comparative estimate of acoustic emission of thin-walled structures excited by a turbulent boundary layer for various representations of the mutual spectrum.
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- Acoustical Physics, 2012, v. 58, n. 4, p. 420, doi. 10.1134/S1063771012040173
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- Article
Acoustic field in a closed layered shell with resonant systems.
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- Acoustical Physics, 2006, v. 52, n. 1, p. 43, doi. 10.1134/S1063771006010064
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- Article
Analysis of the Sound Transmission Loss of Panels with Resonant Systems on the Basis of Equivalent Representations.
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- Acoustical Physics, 2005, v. 51, n. 3, p. 300, doi. 10.1134/1.1922543
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- Article
Correlation of Pressure Fluctuations with Tangential Stresses in a Turbulent Boundary Layer.
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- Acoustical Physics, 2003, v. 49, n. 1, p. 113, doi. 10.1134/1.1537397
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- Article
Sound Transmission Loss of Panels with Resonant Elements.
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- Acoustical Physics, 2001, v. 47, n. 3, p. 291, doi. 10.1134/1.1371584
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- Article