Experimental study of the K-regime of breakdown in straight and swept wing boundary layers

Physics of Fluids

Volumn 13, Issue 7, 2001, Pages 2129-2132

  Chernoray, V G ^a   Bakchinov, A A ^b   Kozlov, V V ^a   Lofdahl L ^b  

^a KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS   (Russian Federation)

^b CHALMERS UNIVERSITY OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; FOURIER TRANSFORMS; TRANSITION FLOW;

FREQUENCY-WAVE NUMBER;

BOUNDARY LAYER FLOW;

AIRCRAFT; AIRFLOW; BOUNDARY LAYER; EXPERIMENTAL STUDY; FLOW FIELD; THREE-DIMENSIONAL FLOW; WING;

EID: 0035398378     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.1366667     Document Type: Article

References (13)

1. Stability of three-dimensional boundary layers
2. The three-dimensional nature of boundary layer instability
3. Nonlinear development of a wave in a boundary layer
4. Forced and unforced subharmonic resonance in boundary layer transition
5. Detailed flow-field observations in the transition process in a thick boundary layer
6. Experimental study of the K-regime breakdown of a laminar boundary layer
7. Secondary instability of boundary layers
8. Direct numerical simulation of controlled transition in a flat-plate boundary layer
9. Formation of three-dimensional structures in a boundary layer at transition
10. Resemblance of K- and N-regimes of boundary layer transition at late stages
11. Numerical simulation of instability and transition in boundary layer flows
12. Numerical simulation of boundary layer transition and transition control
13. Modelling of streaky-structures in two- and three-dimensional boundary layers