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Influence of the Size Variation of Compressor Blades on Gas Dynamics and Strength Characteristics

  • AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT
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Abstract

The size distribution of a set of one-stage stator blades was studied in this work based on the results of 3D scanning of 150 profiles. Based on the obtained data set, the distribution characteristics of the main profile dimensions were determined. An analysis of both strength characteristics and gas dynamics was performed for artificially generated blades.

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Authors and Affiliations

  1. P.I. Baranov Central Institute of Aviation Motors (CIAM), ul. Aviamotornaya 2, 111116, Moscow, Russia

    A. V. Semenov & P. G. Kozhemyako

Authors
  1. A. V. Semenov
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  2. P. G. Kozhemyako
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Correspondence to A. V. Semenov.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 3, pp. 128 - 132.

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Semenov, A.V., Kozhemyako, P.G. Influence of the Size Variation of Compressor Blades on Gas Dynamics and Strength Characteristics. Russ. Aeronaut. 64, 497–502 (2021). https://doi.org/10.3103/S106879982103017X

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  • DOI: https://doi.org/10.3103/S106879982103017X

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