Stability of a four-vortex aircraft wake model

Physics of Fluids

Volumn 12, Issue 10, 2000, Pages 2438-2443

  Fabre, D ^a   Jacquin, L ^a  

^a ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONVERGENCE OF NUMERICAL METHODS; INITIAL VALUE PROBLEMS; PERTURBATION TECHNIQUES; VORTEX FLOW;

FOUR VORTEX AIRCRAFT WAKE MODEL; LARGE SCALE CROW INSTABILITY; VORTEX FILAMENT STABILITY METHOD;

WAKES;

AIRCRAFT; MATHEMATICAL MODELING; VORTEX; WAKE;

EID: 0034306752     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.1289397     Document Type: Article

References (12)

1. Airplane trailing vortices
2. Stability theory for a pair of trailing vortices
3. Theoretical and experimental study of the stability of a vortex pair
4. Spatio-temporal development of the long- and short-wave vortex-pair instabilities
5. Instability and transient growth for two trailing-vortex pairs
6. A method for accelerating the destruction of aircraft wake vortices
7. Motion of a vortex filament with axial flow
8. Bending waves on inviscid columnar vortices
9. Theoretical and numerical analysis of wake vortices