A numerical study of flutter in a transonic fan
The bending mode flutter of a modern rr transonic fan has been studied using a quasi-three-dimensional viscous unsteady CFD code. The type of flutter in this research is that of a highly loaded blade with a tip relative Mach number just above unity, commonly refer red to as transonic stall flutter....
| Main Authors: | , |
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| Format: | Journal article |
| Language: | English |
| Published: |
ASME
1998
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