Complex approach to development the aeroacoustic methods in diagnostics of the flow-through part of gas turbine aviation engines

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In article the complex approach to development the aeroacoustic methods of diagnostics of flow-through part in aviation gas turbine engines on the basis of using the passive fiber-optical and location technologies is considered.

Aeroacoustic methods, diagnostics, fiber-optical distributed sensors, mutual-spectral matrix

Короткий адрес: https://sciup.org/148200625

IDR: 148200625

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