A Comprehensive Solution of the Problems of Ensuring the Strength of Gas Turbine Engine Compressor at the Design Stage

Vedeneev, Vasily; Kolotnikov, M. E.; Mossakovskii, P. A.; Kostyreva, L. A.; Abdukhakimov, F. A.; Макаров, П. В.; Pyhalov, A. A.; Dudaev, M. A.

doi:10.1088/1757-899x/302/1/012079

Cited by 2 publications

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“…It is noteworthy that a similar approach is already successfully used for metals by P.A. Mossakovskii et al to predict the destruction of the GTE during fan blade-out events [81].…”

Section: Basic Recommendations On High-velocity Composite Impact Modementioning

confidence: 99%

Creation and verification of computational models for analysis of the mechanical behaviour of jet engines composite components under high-velocity impact: main problems and basic recommendations

Kudryavtsev

Zhikharev

Olivenko

2019

PNRPU Mechanics Bulletin

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Currently, modern CAE programs like ANSYS, LS-DYNA, ABAQUS, Simcenter 3D etc. are widely used to develop each engineering product. CAE reduces development costs and speeds up product launches. Computer modelling allows eliminating unsuccessful design options at early design stages and minimising or eliminating critical design changes at the prototype testing stage. Computer simulations are especially needed for the development of high-performance perfection designs like jet engines. The use of composites in the engines requires the availability of appropriate design tools to assess the mechanical behaviour of structural elements made of such materials under operational loads and in an emergency. Predictive modelling of the deformation and fracture of the composite fan blades and fan case subjected to dynamic loading cause considerable interest of engineers. As in the case of simulation of shock loading of metals, a model of a composite material must be verified. However, the problem is that the fibrous composite material itself is already a structure and can be modelled in various ways: without considering the layered structure (homogeneous approach) taking the mesostructure into account (at the ply-level or at the yarn-level) taking the microstructure into account (at the filament level). The requirements for the initial data, the number of parameters determined during the verification process, the complexity of creating geometric models will differ in each case. This paper briefly describes the main approaches to the numerical simulation of composite elements under highvelocity impact loading. The main advantages and disadvantages of these approaches are also considered. On the example of the meso-scale approach, the main parameters of the computational models that affect the results of calculations are shown. Based on the obtained data, the main recommendations were formulated on the validation of meso-scale models of composites.

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“…It is noteworthy that a similar approach is already successfully used for metals by P.A. Mossakovskii et al to predict the destruction of the GTE during fan blade-out events [81].…”

Section: Basic Recommendations On High-velocity Composite Impact Modementioning

confidence: 99%