Impact of fluidic chevrons on the turbulence structure of a subsonic jet

Collection of Technical Papers - 3rd AIAA Flow Control Conference

Volumn 3, Issue , 2006, Pages 1437-1449

  Laurendeau, E ^a,b   Bonnet, J P ^a,b   Jordan, P ^a,b   Delville, J ^a,b  

^a UNIVERSITÉ DE POITIERS   (France)

^b Laboratoire d'Etudes Aerodynamiques Poitiers   (France)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW CONTROL; JETS; NOISE ABATEMENT; NOZZLES; TURBULENCE;

HIGH FREQUENCY PENALTY; JET NOZZLES; SECONDARY JETS; SUBSONIC JETS;

SUBSONIC AERODYNAMICS;

EID: 33845271424     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3510     Document Type: Conference Paper

References (9)

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3. Callender, B. and Gutmark, B., A near-field investigation of chevron nozzle mechanisms, AIAA/CEAS Aeroacoustics conference and exhibit 2003-3210.
4. Carabello, B. and Samimy, M., Application of proper orthogonal decomposition to a high speed axisymmetric jet, AIAA 31st Fluid Dynamics Conference, 2001-2783.
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7. Lumley, J.L, The structure of inhomogeneous turbulent flows, Atm. Turb. And Radio Wave Prop. Nauka, Moscow, Yaglom and Tatarsky, pp. 166-178, 1967.
8. Sirovich, L., Turbulence and the dynamics of coherent structures. Part I : coherent structures., Quaterly of Applied Mathematics XLV, 1987.
9. Tinney, C.E. and Glauser M.N., The evolution of the most energetic modes in a high subsonic Mach number turbulent jet, 43rd AIAA Aerospace Sciences Meeting and exhibit, 2005.