Stall Boundary Analysis
Stall Boundary Analysis is a methodological framework within flight envelope characterization that identifies and quantifies the aerodynamic limits of an aircraft's operational envelope where airflow separation leads to loss of lift, distinguishing itself by systematically modeling the onset of stall conditions across varying flight parameters.
13
Publications
484
Citations
41
Authors
20
Institutions
Publications per year
2017–2026
5
Parents
13
1–5 of 13
41
3
h-index
3
h-index
2
h-index
Laboratoire de Mécanique des Fluides et d'Acoustique, France
2 publications · 37 citations
2
h-index
2
h-index
1–5 of 41
20

Imperial College London
London, United Kingdom
5 h-index
10 publications
694 citations
Rolls-Royce (United Kingdom)
London, United Kingdom
3 h-index
3 publications
238 citations

Beihang University
Beijing, China
3 h-index
11 publications
198 citations
Université Claude Bernard Lyon 1
Villeurbanne, France
2 h-index
4 publications
77 citations

Centre National de la Recherche Scientifique
Paris, France
2 h-index
4 publications
77 citations
Laboratoire de Mécanique des Fluides et d'Acoustique
Écully, France
2 h-index
4 publications
77 citations
Institut National des Sciences Appliquées de Lyon
Lyon, France
2 h-index
4 publications
77 citations

École Centrale de Lyon
Écully, France
2 h-index
4 publications
77 citations
1–8 of 20
5 publications · 234 citations
5
h-index
2 publications · 91 citations
2
h-index
Repository · 1 publications · 31 citations
1
h-index
1 publications · 62 citations
1
h-index
IJTPP · 1 publications · 17 citations
1
h-index
1–5