Optimization of blade angles of a nine-stage version of a high-pressure compressor of a supersonic passenger aircraft engine

Author:

Strelets Dmitriy Yu.,Tikhtey Yuriy N.,Kremenchutsky Vladimir V.

Publisher

AIP Publishing

Reference13 articles.

1. Works of leading aircraft engine companies on the creation of advanced aircraft engines (analytical review). Under the general editorship of Doctor of Technical Science Skibin V.A. and Candidate of Technical Science Solonin V.I. (CIAM 2004), p. 424.

2. Substantiation of choosing rational appearance of nose of aircraft with the use of mathematical modeling

3. V. I. Babkin, A. I. Lanshin and A. S. Polev, Creation of competitive aircraft engines in 2025-2030 (CIAM. Intersectoral almanac, 2015) 49, pp. 25–29.

4. Modeling of Product Life Cycle Stages Optimization Taking into Consideration Uncertainty of the Main Parametrical Variables

5. V. I. Babkin and V. I. Solonin, “The role and place of experimental research in the development of advanced aircraft engines,” Engine 4 (100), 2015.

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