A navier-stokes analysis of airfoils in oscillating transonic cascades for the prediction of aerodynamic damping
An unsteady, compressible, two-dimensional, thin shear layer Navier-Stokes solver is modified to predict the motion-dependent unsteady flow around oscillating airfoils in a cascade. A quasi-three-dimensional formulation is used to account for the streamwise variation of streamtube height. The code u...
| Main Authors: | , |
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| Format: | Journal article |
| Language: | English |
| Published: |
1997
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