Linear and nonlinear perturbation analysis of the symmetry breaking in time-periodic propulsive wakes

被引:25
作者
Jallas, Damien [1 ]
Marquet, Olivier [1 ]
Fabre, David [2 ]
机构
[1] Off Natl Etud & Rech Aerosp, French Aerosp Lab, DAAA, 8 Rue Vertugadins, F-92190 Meudon, France
[2] Univ Toulouse, INPT, UPS Inst Mecan Fluides Toulouse IMFT, Allee Camille Soula, F-31400 Toulouse, France
关键词
OSCILLATING CIRCULAR-CYLINDER; FLOQUET STABILITY ANALYSIS; FLOW; FLEXIBILITY; EQUATIONS; AIRFOIL; FLIGHT; MODEL; WAVES;
D O I
10.1103/PhysRevE.95.063111
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
The two-dimensional and time-periodic wake flows produced by a pitching foil are investigated numerically for a fixed flapping amplitude. As the flapping frequency is increased, three regimes are identified in the time-marching nonlinear simulations. The first regime is characterized by nondeviated wake flows with zero time-averaged lift. In the second regime, the wake flow is slightly deviated from the streamwise direction and the time-averaged lift is slightly positive or negative. The third regime is characterized by larger deviations of the wake, associated with larger values of both the time-averaged lift and the thrust. The transition from the first to the second regime is examined by performing a Floquet stability analysis of the nondeviated wake. A specific method is introduced to compute the time-periodic, nondeviated wake when it is unstable. It is found that one synchronous antisymmetric mode becomes unstable at the critical frequency where deviation occurs. Investigation of its instantaneous and time-averaged characteristics show that it acts as a displacement mode translating the nondeviated wake away from the streamwise direction. Finally, it is demonstrated that the transition from the second to the third regime is linked to nonlinear effects that amplify both antisymmetric and symmetric perturbations around the foil.
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页数:15
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