Experimental investigation of the development of secondary perturbations on a swept wing

Fluid Dynamics

Volumn 36, Issue 6, 2001, Pages 909-914

  Kozlov, V V ^a   Sova, V A ^a   Shcherbakov, V A ^a  

^a NONE

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYER; INSTABILITY;

EID: 0035729124     PISSN: 00154628     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1017910609342     Document Type: Article

References (17)

1. Linear stability theory applied to boundary layers
2. Laminar-turbulent transition for a higher degree of free-stream turbulence
3. Görtler vortices
4. On the Görtler instability of boundary layers
5. Secondary instability of wall-bounded shear flow
6. Stability of three-dimensional boundary layers
7. Influence of an acoustic field on the flow structure and the laminar-turbulent transition on a swept wing
8. Generation of streamwise structures in the swept wing boundary layer and their secondary instability
9. Experimental investigation of the process of transition to turbulence on a solitary steady-state perturbation in the swept wing boundary layer
10. Experimental investigation of high-frequency secondary perturbations in the swept wing boundary layer
11. Transition control by riblets in swept wing boundary layer with an embedded streamwise vortex
12. Influence of high-amplitude noise on boundary-layer transition to turbulence
13. Leading-edge roughness as a transition control mechanism
14. Hydrodynamic instability and receptivity of small scale separation regions