|
|
|
|
|
Ashutosh Kumar Singh, Sourabh Kumar and Kuldeep Singh
The recent advancement of cooling methodologies for critical components such as turbine blades, combustor liners, and afterburner liners has led to the development of a combination of impingement and film cooling. The present study proposes an efficient ...
ver más
|
|
|
|
|
|
|
|
|
|
|
Xiaoxia Zheng, Yu Zou, Bohan He, Jixin Xiang, Zhiqiang Li and Qiao Yang
The buckling failure of the afterburner cylinder is a serious safety concern for aero-engines. To tackle this issue, the buckling simulation analysis of the afterburner cylinder was carried out by using finite element method (FEM) software to obtain the ...
ver más
|
|
|
|
|
|
|
|
|
|
|
Kaleab Fetahi, Sharanabasaweshwara A. Asundi and Arthur C. Taylor
Presented herein is a comparative performance analysis of a novel turbofan engine with an auxiliary combustion chamber, nicknamed the TurboAux engine, against a turbojet engine, and a low bypass ratio turbofan engine with an afterburner is presented. The...
ver más
|
|
|
|
|
|
|
|
|
|
|
Lingjun Tu, Zheng Qi, Zhen Wang, Sheng Zhao, Yujie Lu, Weijie Fan, Hao Sun, Xiaofan Wang, Chao Feng and Zhentang Zhao
In this study, we implement attosecond afterburners in an ultrashort soft X-ray free-electron laser (FEL) to improve the performance of generating attosecond pulses. In this scheme, the FEL pulse produced in the normal radiator section is dumped while th...
ver más
|
|
|
|
|
|
|
|
|
|
|
Hideyuki Taguchi, Kenya Harada, Hiroaki Kobayashi, Motoyuki Hongoh, Daisaku Masaki and Shunsuke Nishida
This study investigated a pre-cooled turbojet engine for a Mach 5 class hypersonic transport aircraft. The engine was demonstrated under takeoff and Mach 2 flight conditions, and a Mach 5 propulsion wind tunnel test is planned. The engine is composed of ...
ver más
|
|
|
|
|
|