Pitching Airfoils
Pitching Airfoils is a theoretical construct in unsteady aerodynamics that characterizes the dynamic behavior of an airfoil undergoing time-varying angular oscillations about its pitch axis, distinguishing it from other unsteady aerodynamic phenomena by its focus on the generation of unsteady lift, moment, and vortex shedding due to forced or free rotational motion.
739
Publications
30.4K
Citations
1.4K
Authors
429
Institutions
Publications per year
2017–2026
220
Parents
739
Vortex breakdown on slender sharp-edged wings
W. H. Wentz, D. L. Kohlman · Journal of Aircraft · 1971 · 270 citations
1–5 of 739
1.4K
United States Air Force Research Laboratory, United States
26 publications · 1.3K citations
19
h-index
United States Air Force Research Laboratory, United States
20 publications · 1.1K citations
17
h-index
12
h-index
9
h-index
9
h-index
1–5 of 1.4K
429

Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
20 h-index
38 publications
3.4K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
19 h-index
41 publications
2.3K citations
University of Michigan
Ann Arbor, United States
15 h-index
50 publications
2.5K citations

Ames Research Center
Mountain View, United States
14 h-index
21 publications
937 citations
Princeton University
Princeton, United States
14 h-index
32 publications
3.3K citations

Lehigh University
Bethlehem, United States
14 h-index
34 publications
1.3K citations

Illinois Institute of Technology
Chicago, United States
13 h-index
29 publications
979 citations

University of Glasgow
Glasgow, United Kingdom
12 h-index
39 publications
1.1K citations
1–8 of 429
120 publications · 6.8K citations
47
h-index
46 publications · 3.4K citations
32
h-index
57 publications · 2.7K citations
30
h-index
41 publications · 1.9K citations
24
h-index
42 publications · 1.5K citations
23
h-index
1–5