Flows Around Bodies: Difference between revisions
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| [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10 | | [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10<sup>6</sup>)]] || [[University of Surrey]] | ||
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Revision as of 11:12, 12 May 2009
State-of-the-Art Review
UFR | Underlying Flow Regime | Contributor |
---|---|---|
2-01 | Flow behind a blunt trailing edge | Vrije Universiteit Brussel |
2-02 | Flow past cylinder | Universität Karlsruhe |
2-03 | Flow around oscillating airfoil | Cranfield University |
2-04 | Flow around (airfoils and) blades (subsonic) | NTUA |
2-05 | [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x106)]] | University of Surrey |
2-06 | Flow around (airfoils and) blades (transonic) | Czech Academy of Sciences |
2-07 | 3D flow around blades | ALSTOM Power (Switzerland) Ltd |