Abstract
The principle of dynamic separation and attachment control was demonstrated on a stationary generic flap by periodic excitation. The dynamic separation and attachment were dependent upon excitation frequency and amplitude, flap detection angle, flap length, and inflow conditions. A large-time-scale disparity between the excitation frequencies and airfoil pitching frequencies with respect to rotorcraft was observed.
Original language | English (US) |
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Pages (from-to) | 188-189 |
Number of pages | 2 |
Journal | Journal of Aircraft |
Volume | 38 |
Issue number | 1 |
DOIs | |
State | Published - 2001 |
ASJC Scopus subject areas
- Aerospace Engineering