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- W2031923420 abstract "The dynamic stall of an airfoil with leading edge bubble separation is analyzed. The stall flutter of turbomachine blading may involve periodic growth and collapse of such a bubble. The mathematical model representing the physical problem is presented. A flat plate undergoing harmonic oscillations with time-dependent point of re-attachment is studied for the perturbed aerodynamic reactions and applications to the stall flutter problem." @default.
- W2031923420 created "2016-06-24" @default.
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- W2031923420 date "1978-04-09" @default.
- W2031923420 modified "2023-10-18" @default.
- W2031923420 title "Dynamic Stall of an Airfoil With Leading Edge Bubble Separation Involving Time Dependent Re-Attachment" @default.
- W2031923420 doi "https://doi.org/10.1115/78-gt-194" @default.
- W2031923420 hasPublicationYear "1978" @default.
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