Flight Envelope Loads
Flight Envelope Loads is a structural and aerodynamic load construct that characterizes the extreme and operational forces acting on an aircraft across its entire permissible range of altitude, speed, and maneuver conditions within the flight envelope.
14
Publications
370
Citations
46
Authors
16
Institutions
Publications per year
2017–2026
5
Parents
14
Progress toward CFD for full flight envelope
Edward N. Tinoco, David Bogue, T-J. Kao et al. · The Aeronautical Journal · 2005 · 33 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
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Goodyear (United States)
Akron, United States
1 h-index
1 publications
11 citations
Georgia Institute of Technology
Atlanta, United States
1 h-index
7 publications
91 citations
Airbus (United Kingdom)
Bristol, United Kingdom
1 h-index
1 publications
13 citations
École Polytechnique Fédérale de Lausanne
Lausanne, Switzerland
1 h-index
3 publications
258 citations
Behavioral Tech Research, Inc.
Seattle, United States
1 h-index
6 publications
198 citations

Boeing (United States)
Chicago, United States
1 h-index
6 publications
198 citations

Naval Air Systems Command
NAS Pax River, United States
1 h-index
5 publications
120 citations
Politecnico di Milano
Milan, Italy
1 h-index
3 publications
75 citations
1–8 of 16
4 publications · 63 citations
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1 publications · 86 citations
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1 publications · 33 citations
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1 publications · 24 citations
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Repository · 1 publications · 17 citations
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