Nonlinear Trim
Nonlinear Trim is a computational method used in aerospace engineering to determine equilibrium flight conditions by solving nonlinear systems of equations that model aerodynamic, inertial, and propulsive forces, distinguishing it from linearized trim approaches through its fidelity to complex, real-world vehicle dynamics.
24
Publications
550
Citations
53
Authors
23
Institutions
Publications per year
2017–2026
3
Parents
24
1–5 of 24
53
7
h-index
6
h-index
3
h-index
2
h-index
2
h-index
1–5 of 53
23
Georgia Institute of Technology
Atlanta, United States
8 h-index
18 publications
530 citations
Bihrle Applied Research (United States)
Hampton, United States
2 h-index
4 publications
188 citations
University of California, Los Angeles
Los Angeles, United States
2 h-index
2 publications
36 citations
Florida International University
Miami, United States
2 h-index
6 publications
84 citations
Åbo Akademi University
Turku, Finland
1 h-index
1 publications
40 citations

University of Milan
Milan, Italy
1 h-index
4 publications
64 citations

Sapienza University of Rome
Rome, Italy
1 h-index
1 publications
18 citations
University of Maryland, College Park
College Park, United States
1 h-index
2 publications
56 citations
1–8 of 23
5 publications · 223 citations
5
h-index
3 publications · 48 citations
3
h-index
Conference · 1 publications · 13 citations
1
h-index
1 publications · 40 citations
1
h-index
Conference · 1 publications · 13 citations
1
h-index
1–5