Propeller Integration
Propeller Integration is the systematic incorporation of a propeller system into an aircraft's overall propulsion architecture to ensure optimal aerodynamic performance, structural compatibility, and operational efficiency within the broader context of propulsion system design.
35
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1.3K
Citations
96
Authors
42
Institutions
Publications per year
2017–2026
17
35
Propeller-wing integration for minimum induced loss
Ilan Kroo · Journal of Aircraft · 1986 · 104 citations
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42

Langley Research Center
Hampton, United States
4 h-index
8 publications
188 citations
National Cheng Kung University
Tainan City, Taiwan
2 h-index
8 publications
285 citations

Glenn Research Center
Cleveland, United States
2 h-index
5 publications
146 citations

Northwestern Polytechnical University
Xi'an, China
2 h-index
8 publications
380 citations

University of Glasgow
Glasgow, United Kingdom
1 h-index
2 publications
42 citations

Ames Research Center
Mountain View, United States
1 h-index
1 publications
15 citations
University of Maryland, College Park
College Park, United States
1 h-index
2 publications
50 citations
University of Southern California
Los Angeles, United States
1 h-index
1 publications
25 citations
1–8 of 42
AST · 5 publications · 214 citations
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3 publications · 253 citations
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Repository · 2 publications · 30 citations
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2 publications · 88 citations
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1 publications · 16 citations
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