.... 17 07 2024 26 07 2024 23 08 2024 RDC gas turbine engine Row-1 blade design RDC-turbine integration Traditional swirl stabilized gas turbine combustors used for aerospace and stationary power generation applications utilize the Brayton cycle, wherein...

...-specific fuel consumption (g kN −1 s −1 ) W = mass flow rate (kg s −1 ) w norm = normalized work Y = isentropic parameter for pressure ratio gas turbine engine hydrogen fuel switch engine performance In this century, the main challenge for aviation...

...Ran Ao; Yunpeng Cao; Junqi Luan; Xiaoyu Han; Shuying Li; Li Yan Since the health status of gas turbine engine is difficult to quantify, which brings great challenges to health assessment and remaining useful life predictions. To solve this problem, a gray target calculation and cloud gravity center...

...Foster Kwame Kholi; Jaehyun Park; Kyeongho Lee; Man Yeong Ha; Michael Klingsporn; Jason Chetwynd-Chatwin; Sang Youl Yoon; June Kee Min The fuel-cooled oil cooler (FCOC) in the lubrication circuit plays a critical role in the aero gas-turbine engine's aerothermal management. However, the low...

... October 20, 2013; published online November 27, 2013. Editor: David Wisler. 03 04 2013 20 10 2013 This paper presents the metaheuristic design and optimization of fuzzy-based gas turbine engine (GTE) fuel flow controller by means of a hybrid invasive weed optimization/particle swarm...

... obtained in the first step. The developed Adaptive GPA approach has been tested in four test cases where the performance and degradation of a model gas turbine engine similar to Rolls-Royce aero engine Avon-300 have been analyzed. The case studies have shown that the developed novel linear and nonlinear...

... simulation of a gas turbine engine has been developed. Most of the control design techniques need the linear representation of a plant at various operating points. In this regard, the linear analysis tool box of MATLAB-SIMULINK ( Anon., 2004, SIMULINK: User’s Guide, The Math Works, Inc. ) has been used...