Thrust-to-weight Optimization
Thrust-To-Weight Optimization is a performance-driven engineering methodology within aerospace systems design that specifically involves the systematic adjustment and balancing of an aircraft's thrust output relative to its total weight to achieve optimal acceleration, stability, and efficiency during autonomous takeoff.
24
Publications
958
Citations
85
Authors
35
Institutions
Publications per year
2017–2026
6
Parents
24
1–5 of 24
85
1
h-index
1
h-index
1
h-index
1
h-index
University of Electronic Science and Technology of China, China
1 publications · 63 citations
1
h-index
1–5 of 85
35

Beihang University
Beijing, China
2 h-index
9 publications
242 citations
Ohio Aerospace Institute
Cleveland, United States
1 h-index
1 publications
10 citations

Dalian Maritime University
Dalian, China
1 h-index
3 publications
36 citations
Brownsville Public Library
Brownsville, United States
1 h-index
2 publications
20 citations
Messerschmitt-Bölkow-Blohm (Germany)
Ottobrunn, Germany
1 h-index
1 publications
51 citations
Taizhou University
Taizhou, China
1 h-index
1 publications
11 citations
Nanyang Technological University
Singapore, Singapore
1 h-index
2 publications
22 citations
Marshall Space Flight Center
Redstone Arsenal, United States
1 h-index
2 publications
106 citations
1–8 of 35
5 publications · 297 citations
5
h-index
2 publications · 48 citations
2
h-index
1 publications · 10 citations
1
h-index
1 publications · 24 citations
1
h-index
1 publications · 12 citations
1
h-index
1–5