STRESS-STRAIN ANALYSIS OF COMPOSITE FLANGE OF TYPICAL CASING PART FOR AIRCRAFT ENGINE WITH VARIOUS REINFORCEMENT SCHEMES
The possibility of increasing the static strength of the flange of casing part for aircraft engine by applying different types of carbon fiber reinforced plastic is analyzed with the help of two-dimensional axisymmetric numerical model in ANSYS environment. It is established that it allows to increase the strength for 5-10 percent.