New Innovation of Combustion Chamber by Rotating Components Using CFD Tool

Fuel conservation is very important and popular subject given today’s concern for the operating cost economics in the aviation industry. Several techniques based on energizing the performance, or using in-time modifications of the engine combustion chamber will be studied in this project. This second approach on new designing of combustion chamber by rotational component seems to be promising. Considering a commercial aircraft for example, enhancing the engine regime by using combustion chamber by new innovative ideas and thereby increasing air fuel mixing ratio would most likely lead to fuel economy. Then the various dimensions of the combustor are calculated based on different empirical formulas. The air mass flow is then distributed across the zones of the combustor. The whole combustion chamber is modeled using Gambit, a modeling software and presented. The model is then analyzed using various parameters at various stages and levels to determine the optimized design. The aerodynamic flow characteristics are simulated numerically by means of fluent software suite. This project focuses on the design of a structure for an experimental combustion chamber, which will be studied using the computational fluid dynamic analysis