AIAA-2019-2805: Study of Aircraft with Hybrid Laminar Flow Control Based on Exergy Analysis
Aircraft design (Conference)
2019-01-01
26 pages
Conference paper
English
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DataCite | 1899
Conceptual Wing Design Methodology for Aircraft with Hybrid Laminar Flow Control (AIAA 2014-0023)
British Library Conference Proceedings | 2014
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