Rotor Trim Analysis
Rotor Trim Analysis is a computational methodology in rotorcraft aerodynamics that determines the steady-state flight conditions and control inputs required to achieve equilibrium in forces and moments by iteratively adjusting rotor collective and cyclic pitch angles, fuselage orientation, and flight velocity while satisfying aerodynamic, inertial, and propulsive balance constraints.
39
Publications
1.2K
Citations
98
Authors
30
Institutions
Publications per year
2017–2026
9
Parents
39
1–5 of 39
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30

Langley Research Center
Hampton, United States
5 h-index
6 publications
86 citations
University of Maryland, College Park
College Park, United States
5 h-index
8 publications
213 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
4 h-index
13 publications
239 citations

Beihang University
Beijing, China
2 h-index
6 publications
93 citations

University of Glasgow
Glasgow, United Kingdom
2 h-index
4 publications
640 citations

Ames Research Center
Mountain View, United States
2 h-index
3 publications
149 citations

Pennsylvania State University
State College, United States
2 h-index
5 publications
144 citations

Washington University in St. Louis
St Louis, United States
2 h-index
4 publications
110 citations
1–8 of 30
6 publications · 133 citations
6
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5 publications · 242 citations
5
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4 publications · 85 citations
4
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2 publications · 32 citations
2
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AST · 2 publications · 46 citations
2
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1–5