Trim Analysis
Trim Analysis is a systematic computational or analytical method employed within aircraft performance and stability studies to determine the equilibrium flight conditions under which all aerodynamic, inertial, and propulsion forces and moments balance, enabling steady or prescribed maneuvering flight.
54
Publications
2.4K
Citations
138
Authors
63
Institutions
Publications per year
2017–2026
15
54
1–5 of 54
138
4
h-index
3
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2
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Massachusetts Institute of Technology, United States
2 publications · 82 citations
2
h-index
1–5 of 138
63
Nanyang Technological University
Singapore, Singapore
3 h-index
5 publications
108 citations

Ames Research Center
Mountain View, United States
3 h-index
8 publications
991 citations

Indian Institute of Technology Bombay
Mumbai, India
3 h-index
6 publications
169 citations
Georgia Institute of Technology
Atlanta, United States
3 h-index
9 publications
252 citations
Massachusetts Institute of Technology
Cambridge, United States
2 h-index
6 publications
300 citations
University of California, Davis
Davis, United States
2 h-index
2 publications
323 citations

Sharif University of Technology
Tehran, Iran
2 h-index
4 publications
50 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
2 h-index
7 publications
147 citations
1–8 of 63
9 publications · 317 citations
9
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Conference · 2 publications · 31 citations
2
h-index
2 publications · 203 citations
2
h-index
Conference · 2 publications · 27 citations
2
h-index
2 publications · 72 citations
2
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1–5