DEFINITION OF CARBON/CARBON (C/C) COMPOSITE MATERIAL FOR JET ENGINE TURBINE BLADE MODEL IN ANSYS AND EVALUATION OF THERMAL ANALYSIS RESULTS: CALCULATION OF FLOW, PRESSURE, AND EFFICIENCY VALUES IN MATLAB

JET MOTORU TÜRBİN KANATÇIK MODELİNE ANSYS PROGRAMINDA KARBON/KARBON (C/C) KOMPOZİT MALZEME TANIMLANMASI VE TERMAL ANALİZ SONUÇLARININ DEĞERLENDİRİLMESİ: MATLAB PROGRAMINDA AKIŞ, BASINÇ VE VERİMLİLİK DEĞERLERİNİN HESAPLANMASI

Özet

In the design of jet engine turbine blades, various analysis methods such as SOLIDWORKS and ANSYS are used in the literature. The nozzle and temperature analysis of jet engine turbine blades play a crucial role in evaluating the engine's performance, efficiency, and durability. This research article; investigates how carbon/carbon (C/C) composite materials and design parameters (temperature, pressure, and nozzle velocity) affect the durability and performance of turbine blades. A three-dimensional solid model of the turbine blade was created using the ANSYS program. Subsequently, temperature effects were calculated using the MATLAB program. Initially, the C/C composite material assignment was made. Then, temperature values were taken in Kelvin (K) units in the MATLAB program. Three different temperature values, 979.02 K, 1395.62 K, and 3195.62 K, were entered. It was observed that the C/C composite material withstands high temperatures well. In turbine jet engines, an increase in temperature was observed to increase turbine nozzle velocity.