DNS analysis of shock wave / turbulent boundary layer interaction at M = 2.25

4th International Symposium on Turbulence and Shear Flow Phenomena

Volumn 3, Issue , 2005, Pages 1207-1211

  Pirozzoli, Sergio ^a   Grasso, Francesco ^a   Gatski, Thomas B ^b  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADVERSE PRESSURE GRADIENT; BOUNDARY LAYER THICKNESS; BOUNDARY-LAYER SEPARATION; FIELD DYNAMICS; FLAPPING MOTION; INTERACTION ZONE; LENGTH SCALE; REFLECTED SHOCKS; SHOCK ANGLE; TURBULENT BOUNDARY-LAYER INTERACTIONS; UNIVERSAL BEHAVIORS; VORTICAL STRUCTURES;

BOUNDARY LAYER FLOW;

SHEAR FLOW;

EID: 79955906507     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Adams, N. A., 2000, "Direct numerical simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reg = 1685," J. Fluid Mech., Vol. 420, pp. 47-83.
2. Deleuze, J., 1995, "Structure d'une couche limite soumise à une onde de choc incidente," Thèse de doctorat, Université Aix-Marseille II.
3. Garnier, E., Sagaut, P., and Deville, M., 2002, "Large eddy simulation of shock/boundary layer interaction," AIAA J., Vol. 40, pp. 1935-1944.
4. Laurent, H., 1996, "Turbulence d'une interaction onde de choc / couche limite sur une paroi adiabatique ou chauffée," Thèse de doctorat, Université Aix-Marseille II.
5. Na, Y., and Moin, P., 1998, "Direct numerical simulation of a separated turbulent boundary layer," J. Fluid Mech., Vol. 374, pp. 379-405.
6. Pirozzoli, S., Grasso, F., and Gatski, T. B., 2004, "Direct numerical simulation and analysis of a spatially evolving turbulent boundary layer at M = 2.25," Phys. Fluids, Vol. 16, pp. 530-545.
7. Smits, A. J., and Dussauge, J. P., 1996, Turbulent shar layers in supersonic flow, American Institute of Physics, New York.
8. White, F. M., 1974, Viscous fluid flow, McGraw-Hill, New York.