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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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dc.date July 1, 1972 en_US
dc.date.accessioned 2010-04-26T23:34:23Z
dc.date.available 2010-04-26T23:34:23Z
dc.date.issued 2010-04-26T23:34:23Z
dc.identifier 3424-2 en_US
dc.identifier.other 39080027537205 en_US
dc.identifier.uri http://hdl.handle.net/1721.3/52288
dc.title Application of the Method of Integral Relations (MIR) to Transonic Airfoil Problems, Part II - Inviscid Supercritical Flow about Lifting Airfoils with Embedded Shock Wave en_US


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