AIAA-2019-2805: Study of Aircraft with Hybrid Laminar Flow Control Based on Exergy Analysis
Aircraft design (Conference)
01.01.2019
26 pages
Aufsatz (Konferenz)
Englisch
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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
|British Library Conference Proceedings | 2014
|Kraftfahrwesen | 1979
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