A complete mathematical model is formulated to analyse the effects of mean flow incidence angle on the unsteady aerodynamics of an oscillating airfoil in an incompressible flow field. A velocity potential formulation is utilized. The steady flow is independent of the unsteady flow field. However, th
โฆ LIBER โฆ
Prediction of oscillating thick cambered aerofoil aerodynamics by a locally analytic method
โ Scribed by Hsiao-Wei D. Chiang; Sanford Fleeter
- Publisher
- John Wiley and Sons
- Year
- 1988
- Tongue
- English
- Weight
- 867 KB
- Volume
- 8
- Category
- Article
- ISSN
- 0271-2091
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