Flight Envelope Analysis
Flight Envelope Analysis is a systematic methodological framework in missile flight dynamics that characterizes the operational limits of a missile’s achievable flight conditions by defining the boundaries of its aerodynamic, propulsive, and structural performance under varying atmospheric and kinematic constraints.
310
Publications
8K
Citations
791
Authors
222
Institutions
Publications per year
2017–2026
60
Parents
310
Parametric Uncertainty Modeling using LFTs
Paul Lambrechts, Jan Terlouw, Samir Bennani et al. · 1993 · 100 citations
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Langley Research Center
Hampton, United States
16 h-index
56 publications
1.1K citations

Ames Research Center
Mountain View, United States
11 h-index
15 publications
487 citations
Georgia Institute of Technology
Atlanta, United States
9 h-index
18 publications
336 citations

Delft University of Technology
Delft, The Netherlands
9 h-index
31 publications
892 citations
Lockheed Martin (United States)
Bethesda, United States
7 h-index
14 publications
578 citations

Naval Surface Warfare Center
Washington, United States
7 h-index
16 publications
240 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
6 h-index
21 publications
291 citations

Armstrong Flight Research Center
Edwards, United States
6 h-index
8 publications
359 citations
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38 publications · 715 citations
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21 publications · 926 citations
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21 publications · 539 citations
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AST · 17 publications · 561 citations
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Repository · 7 publications · 119 citations
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