Optimization of the Number, Distribution of Work by Stages, and Solidity of Profile Vane Cascades during Compressor Design

Author:

Krivosheev I. A.,Rozhkov K. E.,Simonov N. B.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference14 articles.

1. Belousov, A.N., Musatkin, N.F., and Rad’ko, V.M., Teoriya i raschet aviatsionnykh lopatochnykh mashin (Theory and Calculation of Aviation Impeller Machines), Samara: Izd. Samarskogo Gos. Aerokosmich. Univ., 2003.

2. Emin, O.N., Karasev, V.N., and Rzhavin, Yu.A., Vybor parametrov i gazodinamicheskii raschet osevykh kompressorov i turbin aviatsionnykh GTD (Selection of Parameters and Gas-Dynamic Calculation of Axial Compressors and Turbines for Aircraft GTEs), Moscow: MAI, 2003.

3. Kholshchevnikov, K.V., Teoriya i raschet aviatsionnykh lopatochnykh mashin (Theory and Design of Aircraft Turbomachines), Moscow: Mashinostroenie, 1970.

4. Bunimovich, A.I. and Svyatogorov, A.A., Aerodynamic Characteristics of Compressor Blade Planes at High Subsonic Speed, in Lopatochnye mashiny i struinye apparaty (Impeller Machines and Jet Devices), Moscow: Mashinostroenie, 1967, issue 2, pp. 5–35.

5. Komissarov, G.A., Mikir’chan, V.M., and Khait, M.V., A Technique for the Gas Dynamic Calculation of the Axial Compressor, Technical Report TsIAM, Moscow: TsIAM, 1961.

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