Angle of Attack Dynamics is a longitudinal flight dynamics construct that characterizes the time-varying behavior of the angle between the aircraft’s oncoming airflow and its reference chord line, distinguishing itself from other aerodynamic state dynamics by directly governing lift generation and stall onset mechanisms.
256
Publications
8.6K
Citations
599
Authors
211
Institutions
Publications per year
2017–2026
34
Parents
Publications
256
1–5 of 256
Authors
599
- NJ
7
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- LB
6
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- JB
4
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- LR
4
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- AK
4
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1–5 of 599
Institutions
211
Langley Research Center
Hampton, United States
16 h-index
39 publications
819 citations
Ames Research Center
Mountain View, United States
11 h-index
19 publications
675 citations
Virginia Tech
Blacksburg, United States
7 h-index
15 publications
427 citations
Armstrong Flight Research Center
Edwards, United States
6 h-index
9 publications
145 citations
Northwestern Polytechnical University
Xi'an, China
6 h-index
18 publications
493 citations
Harbin Institute of Technology
Harbin, China
6 h-index
17 publications
631 citations
United States Air Force Research Laboratory
Wright-Patterson AFB, United States
5 h-index
11 publications
505 citations
Stanford University
Stanford, United States
5 h-index
10 publications
319 citations
1–8 of 211
Venues
- Journal of Aircraft
31 publications · 1.2K citations
17
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- AIAA Journal
18 publications · 469 citations
15
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- NASA Technical Reports Server (NASA)
Repository · 11 publications · 205 citations
11
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- Journal of Guidance Control and Dynamics
10 publications · 823 citations
10
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- Aerospace Science and Technology
AST · 7 publications · 345 citations
7
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1–5