Trim Condition Analysis
Trim Condition Analysis is a methodological framework within longitudinal flight dynamics that identifies and evaluates steady-state equilibrium conditions of an aircraft’s motion by determining the specific control and state variable settings that balance all forces and moments, thereby enabling stable and unaccelerated flight.
36
Publications
1.1K
Citations
107
Authors
43
Institutions
Publications per year
2017–2026
9
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107
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43

Langley Research Center
Hampton, United States
3 h-index
10 publications
173 citations

Drexel University
Philadelphia, United States
2 h-index
4 publications
56 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
2 h-index
3 publications
334 citations
The University of Texas at Arlington
Arlington, United States
2 h-index
5 publications
88 citations
Middle East Technical University
Ankara, Türkiye
2 h-index
6 publications
75 citations

Harbin Institute of Technology
Harbin, China
2 h-index
10 publications
430 citations
Nanyang Technological University
Singapore, Singapore
1 h-index
1 publications
50 citations

Turkish Armed Forces
Çankaya, Turkey
1 h-index
2 publications
30 citations
1–8 of 43
7 publications · 168 citations
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Conference · 2 publications · 31 citations
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2 publications · 78 citations
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2 publications · 61 citations
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Conference · 1 publications · 13 citations
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