Complex seal designing as element of air secondary system in aircraft engine

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In article the algorithm of seal designing as element in common air secondary system of the engine is considered. The algorithm combines accounts of hydraulic resistance, thermal condition, stress and deformation condition, aircraft engines parameters in different program complexes.

Air secondary system, seal, efficiency, technique, algorithm, leakage

Короткий адрес: https://sciup.org/148200491

IDR: 148200491

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