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A boundary integral equations approach for the study of the subsonic compressible flow past a cusped airfoil

✍ Scribed by Adrian Carabineanu

Publisher: Elsevier Science
Year: 1997
Tongue: English
Weight: 275 KB
Volume: 30
Category: Article
ISSN: 0362-546X
DOI: 10.1016/s0362-546x(96)00359-8

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✦ Synopsis

We study the subsonic steady Id lifting flow around airfoils with nlsped trailing edge using the Imai-Lamb-lacoh asymptotic method coupled with the boundary integral equations method.

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