Research on the Application of Integrated Design on Micro Turbojet Engine
There are no detailed design criteria and methods for the integrated design of micro turbojet engine.The size and weight design and evaluation method for turbojet engines are used to perform the integrated design of several 9~80 kgf micro turbojet engines and evaluate the engines'data.The integ...
Main Authors: | CHEN Minze, CHEN Yuchun, JIA Linyuan, HUANG Xinchun, LI Sunyang |
---|---|
Format: | Article |
Language: | zho |
Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2022-08-01
|
Series: | Hangkong gongcheng jinzhan |
Subjects: | |
Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021149 |
Similar Items
-
Intensification of convective heat exchange of walls of heat pipe of 3D-printed micro-sized turbojet engine
by: A. V. Pobelyansky, et al.
Published: (2022-03-01) -
Optimum Design of Injection Ring for Micro-turbojet Engine
by: Tan Kun, et al.
Published: (2018-08-01) -
Single Neural Adaptive PID Control for Small UAV Micro-Turbojet Engine
by: Wei Tang, et al.
Published: (2020-01-01) -
Mach 4 Simulating Experiment of Pre-Cooled Turbojet Engine Using Liquid Hydrogen
by: Hideyuki Taguchi, et al.
Published: (2022-01-01) -
Impact of Using Chevrons Nozzle on the Acoustics and Performances of a Micro Turbojet Engine
by: Grigore Cican, et al.
Published: (2021-06-01)