Transonic Control Surface Behavior is a mechanical aerodynamic phenomenon characterized by the dynamic response and stability of aircraft control surfaces operating in the transonic flow regime, where localized supersonic flows and shock wave formations induce nonlinear aerodynamic forces and potential instabilities distinct from those observed in purely subsonic or supersonic conditions.
8
Publications
126
Citations
14
Authors
5
Institutions
Publications per year
2017–2026
0
Parents
Publications
8
1–5 of 8
Authors
14
- MC
2
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- BK
2
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- GSGeorge S. Pick
Naval Facilities Engineering Systems Command, United States
1 publications · 17 citations
1
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- DA
1
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- RI
1
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1–5 of 14
Institutions
5
Ames Research Center
Mountain View, United States
2 h-index
3 publications
56 citations
Langley Research Center
Hampton, United States
2 h-index
7 publications
91 citations
Naval Medical Research Command
Silver Spring, United States
1 h-index
1 publications
17 citations
Northwestern Polytechnical University
Xi'an, China
1 h-index
3 publications
54 citations
HRL Laboratories (United States)
Malibu, United States
1 h-index
1 publications
13 citations
University of Glasgow
Glasgow, United Kingdom
1 publications
12 citations
University of Liverpool
Liverpool, United Kingdom
1 publications
12 citations
1–7 of 5
Venues
- Journal of Aircraft
3 publications · 48 citations
3
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- Journal of Spacecraft and Rockets
1 publications · 17 citations
1
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- Journal of Fluids and Structures
1 publications · 18 citations
1
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- AIAA Journal
1 publications · 18 citations
1
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- 31st Structures, Structural Dynamics and Materials Conference
Conference · 1 publications · 13 citations
1
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1–5