Methodology of Computer-Aided Design of Variable Guide Vanes of Aircraft Engines

APA 6th edition
In-text: (Falaleev & Gvozdev, 2016)
Your Bibliography: Falaleev, S.V. & Gvozdev, V.S.M.a.A.S. (2016). Methodology of Computer-Aided Design of Variable Guide Vanes of Aircraft Engines. International Journal of Environmental and Science Education, 11(10), 3847-3860.

Harvard
In-text: (Falaleev and Gvozdev, 2016)
Your Bibliography: Falaleev, S. and Gvozdev, V. (2016). Methodology of Computer-Aided Design of Variable Guide Vanes of Aircraft Engines. International Journal of Environmental and Science Education, 11(10), pp. 3847-3860.

Chicago 16th edition
In-text: (Falaleev and Gvozdev 2016)
Your Bibliography: Falaleev, Sergei V. and Vladimir S. Melentjev and Alexander S. Gvozdev (2016). "Methodology of Computer-Aided Design of Variable Guide Vanes of Aircraft Engines". International Journal of Environmental and Science Education 11 (10):3847-3860.

Abstract

The paper presents a methodology which helps to avoid a great amount of costly experimental research. This methodology includes thermo-gas dynamic design of an engine and its mounts, the profiling of compressor flow path and cascade design of guide vanes. Employing a method elaborated by Howell, we provide a theoretical solution to the task of assessing the influence of the VGV blades’ angle of rotation on the characteristic of a compressor. The finite element model of a VGV blade helps to solve some problems of strength and tune-out of resonance in the domain of a compressor’s operating frequencies as well as the problem of determining the position of the pressure center and the location of a blade’s pivotal point. Cinematic and dynamic analysis of the control linkage of VGVs is carried out in a MSC.ADAMS package. The investigation is based on geometric 2D and 3D models, gas-dynamic and strength analysis taking into account geometrical nonlinearity and based on the finite element method. The study is also based on the dynamic analysis according to the Euler-Lagrange equation, which describes the behavior of mechanical systems comprised of markers and the Craig-Bampton method implying the theory of superposition of vibrational modes.

Keywords: Howell’s method, methodology of design, turbine airfoil, strength calculation, thermo-gas dynamic analysis

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