SwePub
Sök i LIBRIS databas

  Extended search

WFRF:(Andersson Niklas 1976)
 

Search: WFRF:(Andersson Niklas 1976) > Large-Eddy Simulati...

Large-Eddy Simulation of Subsonic Turbulent Jets and Their Radiated Sound

Andersson, Niklas, 1976 (author)
Chalmers tekniska högskola,Chalmers University of Technology
Eriksson, Lars-Erik, 1950 (author)
Chalmers tekniska högskola,Chalmers University of Technology
Davidson, Lars, 1957 (author)
Chalmers tekniska högskola,Chalmers University of Technology
 (creator_code:org_t)
2005
2005
English.
In: AIAA Journal. ; 43:9, s. 1899-1912
  • Journal article (peer-reviewed)
Abstract Subject headings
Close  
  • Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two jets were simulated, an isothermal jet and a jet with a higher temperature than the quiescent surrounding air. The Mach number was in both cases 0.75 and the jet Reynolds number was 50,000. Sound pressure levels in far-field observer locations were evaluated using Kirchhoff surface integration. The Favre filtered Navier-Stokes equations were solved using a finite volume method solver with a low-dissipation third-order upwind scheme for the convective fluxes, a second-order centered difference approach for the viscous fluxes and a three-stage second-order Runge-Kutta technique in time. The computational domain was discretized using a block structured boundary fitted mesh with approximately 3,000,000 cells. The calculations were performed on a parallel computer, using message-passing interface (MPI). A compressible form of Smagorinsky's subgrid scale model was used for computation of the subgrid scale stresses. Absorbing boundary conditions based on characteristic variables were adopted for all free boundaries. Velocity components specified at the entrainment boundaries were estimated from corresponding Reynolds Averaged Navier-Stokes (RANS) calculations, which enable the use of a rather narrow domain. This, furthermore, ensures that the correct amount of fluid is entrained into the domain. Two-point space-time correlations were obtained for locations in the shear layer center, from which length and time scales of turbulence structures were evaluated. Predicted near-field flow statistics and far-field sound pressure levels (SPL) are both in good agreement with experiments. Predicted (SPL) are for all observers locations, where evaluated, within a 3.0 [dB] deviation from measured levels and for most locations within a 1.0 [dB] deviation. Experimental data used for validation were provided by Laboratoire dEtude Aeròdynamiques, Poiters, France.

Subject headings

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Strömningsmekanik och akustik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Fluid Mechanics and Acoustics (hsv//eng)

Keyword

Jet noise
LES

Publication and Content Type

art (subject category)
ref (subject category)

Find in a library

To the university's database

Find more in SwePub

By the author/editor
Andersson, Nikla ...
Eriksson, Lars-E ...
Davidson, Lars, ...
About the subject
ENGINEERING AND TECHNOLOGY
ENGINEERING AND ...
and Mechanical Engin ...
and Fluid Mechanics ...
Articles in the publication
By the university
Chalmers University of Technology

Search outside SwePub

Kungliga biblioteket hanterar dina personuppgifter i enlighet med EU:s dataskyddsförordning (2018), GDPR. Läs mer om hur det funkar här.
Så här hanterar KB dina uppgifter vid användning av denna tjänst.

 
pil uppåt Close

Copy and save the link in order to return to this view