Engine Matching
Engine Matching is a methodological framework in aerospace engineering that systematically aligns the performance characteristics of gas turbine engines—such as thrust, specific fuel consumption, and operability limits—with the aerodynamic, mission, and design requirements of an aircraft to ensure optimal integration and efficiency across operational regimes.
31
Publications
845
Citations
80
Authors
31
Institutions
Publications per year
2017–2026
17
31
1–5 of 31
80
2
h-index
2
h-index
2
h-index
2
h-index
2
h-index
1–5 of 80
31

Beijing Institute of Technology
Beijing, China
4 h-index
10 publications
151 citations

Imperial College London
London, United Kingdom
2 h-index
7 publications
306 citations
Chongqing University of Technology
Chongqing, China
2 h-index
2 publications
38 citations
Iğdır Üniversitesi
Iğdır, Türkiye
2 h-index
3 publications
75 citations
Naval University of Engineering
Wuhan, China
2 h-index
2 publications
35 citations
Academy of Military Transportation
Tianjin, China
2 h-index
11 publications
195 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
2 h-index
8 publications
180 citations

Rivers State University
Port Harcourt, Nigeria
2 h-index
5 publications
84 citations
1–8 of 31
3 publications · 73 citations
3
h-index
2 publications · 60 citations
2
h-index
CJA · 2 publications · 127 citations
2
h-index
2 publications · 26 citations
2
h-index
JPEE · 2 publications · 34 citations
2
h-index
1–5