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