Active-control system for breakup of airplane trailing vortices

AIAA Journal

Volumn 39, Issue 12, 2001, Pages 2374-2381

  Crouch, J D ^a   Miller, G D ^a   Spalart, P R ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; COMPUTER SIMULATION; LIFT; PERTURBATION TECHNIQUES; WAKES; WIND TUNNELS; WINGS;

VORTEX BREAKUP;

VORTEX FLOW;

EID: 0035662527     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1244     Document Type: Article

References (14)

1. Lift-generated vortex wakes of subsonic transport aircraft
2. Lifespan of trailing vortices in a turbulent atmosphere
3. Stability theory for a pair of trailing vortices
4. Aircraft wake dissipation by sinu-soidal instability and vortex breakdown
5. Instability and transient growth for two trailing-vortex pairs
6. Wake hazard alleviation associated with roll oscillations of wake-generating aircraft
7. Wake vortex attenuation flight tests: A status report
8. Method for accelerating the destruction of aircraft wake vortices
9. Airplane flow-field measurements
10. Fourier/Chebyshev methods for the incompressible Navier-Stokes equations in infinite domains