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Published in 2019 at "AIAA Journal"
DOI: 10.2514/1.j058011
Abstract: This paper presents a combined experimental and computational study of a low-sweep transonic natural laminar flow (NLF) wing with shock-control bumps (SCBs). A transonic NLF wing with a relatively ...
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Keywords:
sweep transonic;
shock control;
low sweep;
laminar flow ... See more keywords