Research on the Flutter of Axial-Turbomachine Blading.
STEVENS INST OF TECH HOBOKEN N J DEPT OF MECHANICAL ENGINEERING
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Theoretical and experimental phases of a program to study flutter in turbomachinery blading are summarized. A general analytical method for predicting the aerodynamic characteristics of partly stalled airfoil is introduced and agrees with experimental results. The effect of location of rotation axis on quasistatic aerodynamic moment is displayed and generalized conclusions are drawn. Author
- Non-electrical Energy Conversion
- Fluid Mechanics