Rotorcraft Trim
Rotorcraft Trim is a dynamic equilibrium condition in which a rotorcraft maintains steady, unaccelerated flight at a constant attitude and velocity with all control inputs and rotor system states held constant.
21
Publications
627
Citations
46
Authors
15
Institutions
Publications per year
2017–2026
4
Parents
21
1–5 of 21
46
3
h-index
3
h-index
2
h-index
2
h-index
1
h-index
1–5 of 46
15

Langley Research Center
Hampton, United States
3 h-index
4 publications
159 citations

Pennsylvania State University
State College, United States
2 h-index
2 publications
35 citations
University of Maryland, College Park
College Park, United States
2 h-index
4 publications
132 citations

Washington University in St. Louis
St Louis, United States
2 h-index
4 publications
110 citations

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

Glasgow Caledonian University
Glasgow, United Kingdom
1 h-index
1 publications
11 citations

Beihang University
Beijing, China
1 h-index
3 publications
39 citations
University of Stuttgart
Stuttgart, Germany
1 h-index
5 publications
160 citations
1–8 of 15
6 publications · 136 citations
6
h-index
3 publications · 94 citations
3
h-index
2 publications · 45 citations
2
h-index
1 publications · 19 citations
1
h-index
1 publications · 13 citations
1
h-index
1–5