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Application of the Method of Integral Relations (MIR) to Transonic Airfoil Problems, Part II - Inviscid Supercritical Flow about Lifting Airfoils with Embedded Shock Wave

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DownloadDTMB_1972_3424_2.pdf (10.65Mb)
URI
http://hdl.handle.net/1721.3/52288
Date
2010-04-26T23:34:23Z
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