Distributed Propulsion Configuration
Distributed Propulsion Configuration is an aircraft propulsion architecture in which multiple propulsors are integrated at distinct locations along the airframe to actively manipulate aerodynamic performance through synergistic interaction between the propulsive flow and the surrounding airflow.
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2K
Citations
159
Authors
47
Institutions
Publications per year
2017–2026
19
46
Amir S. Gohardani · Progress in Aerospace Sciences · 2012 · 84 citations
Engineering, Aerospace Engineering, Electrical Engineering +17
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Cranfield University
Cranfield, United Kingdom
7 h-index
19 publications
550 citations

Langley Research Center
Hampton, United States
7 h-index
18 publications
1.6K citations

Glenn Research Center
Cleveland, United States
4 h-index
12 publications
814 citations

Delft University of Technology
Delft, The Netherlands
3 h-index
10 publications
222 citations
Virginia Tech
Blacksburg, United States
3 h-index
13 publications
623 citations
Empirical Systems Aerospace (United States)
San Luis Obispo, United States
3 h-index
6 publications
429 citations
University of Illinois Urbana-Champaign
Urbana, United States
3 h-index
7 publications
217 citations
Rolling Hills Research (United States)
El Segundo, United States
2 h-index
2 publications
84 citations
1–8 of 47
Conference · 3 publications · 341 citations
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2 publications · 36 citations
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2 publications · 51 citations
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2 publications · 42 citations
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2 publications · 76 citations
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