Large Eddy Simulation for the Analysis of Supersonic Jet Noise Suppression Devices
Doktorsavhandling, 2010
fluidic injection
mixer-ejector
jet noise
Kirchhoff
forward flight effects
LES
acoustic liner
supersonic turbulent jets
broadband time-domain impedance boundary condition
chevrons
shock-associated noise
CAA
aeroacoustics
Författare
Markus Olander Burak
Chalmers, Tillämpad mekanik, Strömningslära
LES based jet noise prediction for mixer-ejector configurations including acoustic liner model
Inter-Noise 2006 Congress, Honolulu, Hawaii, USA,;(2006)
Övrigt konferensbidrag
Near-Field Jet Noise from a Supersonic C-D Chevron Nozzle
16th AIAA/CEAS Aeroacoustics Conference, 7-9 June, Stockholm, Sweden,;(2010)
Övrigt konferensbidrag
Flow and noise predictions for a mixer-ejector engine configuration using LES
;(2007)
Paper i proceeding
Experimental and Numerical Investigation of a Supersonic C-D Nozzle
15th AIAA/CEAS Aeroacoustics Conference, 11-13 May, Miami, Florida,;(2009)
Övrigt konferensbidrag
Micro-Jet Flow Control for Noise Reduction of a Supersonic Jet from a Practical C-D Nozzle
16th AIAA/CEAS Aeroacoustics Conference, 7-9 June, Stockholm, Sweden,;(2010)
Övrigt konferensbidrag
Supersonic Jet Noise from a Conical C-D Nozzle with Forward Flight Effects
47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, , 5-8 January, Orlando, Florida,;(2009)
Övrigt konferensbidrag
Comparison of Flow Control Methods Applied to Conical C-D Nozzles
16th AIAA/CEAS Aeroacoustics Conference, 7-9 June, Stockholm, Sweden,;(2010)
Övrigt konferensbidrag
Experimental and Numerical Investigation of a Supersonic C-D Chevron Nozzle
39th AIAA Fluid Dynamics Conference, 22-25 June, San Antonio, Texas,;(2009)
Övrigt konferensbidrag
Experimental and Numerical Investigation of a Novel Acoustic Liner Concept
16th AIAA/CEAS Aeroacoustics Conference, 7-9 June, Stockholm, Sweden,;(2010)
Övrigt konferensbidrag
Validation of a Time- and Frequency-Domain Grazing Flow Acoustic Liner Model
AIAA Journal,;Vol. 47(2009)p. 1841-1848
Artikel i vetenskaplig tidskrift
Forward Flight Effects on the Shock Structure From a Chevron C-D Nozzle
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 4-7 January, Orlando, Florida,;(2010)
Övrigt konferensbidrag
Ämneskategorier
Strömningsmekanik och akustik
ISBN
978-91-7385-459-7
Doktorsavhandlingar vid Chalmers tekniska högskola. Ny serie: 3140
HC2
Opponent: Prof. Paul G. Tucker, Rank Professor of Turbomachinery Computational Aerodynamics, The University of Cambridge, Whittle Laboratory, England