New research and concepts in turbo‐jet engine design
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 December 1997
Abstract
Presents a brief overview of some new concepts and research results concerning aerodynamic computation and design of jet‐propulsion engines with emphasis on turbomachinery (TM) developed in China, without any attempt to be exhaustive.
Keywords
Citation
Liu, G. and He, J. (1997), "New research and concepts in turbo‐jet engine design", Aircraft Engineering and Aerospace Technology, Vol. 69 No. 6, pp. 527-533. https://doi.org/10.1108/00022669710185986
Publisher
:MCB UP Ltd
Copyright © 1997, MCB UP Limited