Stability Configuration
Stability Configuration is a method within the field of aircraft configuration design that systematically integrates aerodynamic, inertial, and control surface parameters to achieve desired static and dynamic stability characteristics in an aircraft’s flight envelope.
6
Publications
131
Citations
16
Authors
6
Institutions
Publications per year
2017–2026
3
6
Limping following limb loss increases locomotor stability
Simon Wilshin, Paul S. Shamble, Kyle J. Hovey et al. · Journal of Experimental Biology · 2018 · 27 citations · Full text
Engineering, Biology, Zoology +17
1–5 of 6
16
2
h-index
1
h-index
1
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
1 publications · 17 citations
1
h-index
1
h-index
1–5 of 16
6

Ain Shams University
Cairo, Egypt
2 h-index
3 publications
83 citations

University of London
London, United Kingdom
1 h-index
2 publications
54 citations
Temple University
Philadelphia, United States
1 h-index
4 publications
108 citations

Langley Research Center
Hampton, United States
1 h-index
1 publications
22 citations

Royal Veterinary College
London, United Kingdom
1 h-index
2 publications
54 citations

John Carroll University
University Heights, United States
1 h-index
1 publications
27 citations
1–6 of 6
Repository · 2 publications · 37 citations
2
h-index
1 publications · 27 citations
1
h-index
1 publications · 33 citations
1
h-index
Repository · 1 publications · 17 citations
1
h-index
1–4