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000783216 001__ 783216
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000783216 0247_ $$2ISBN$$a978-1-60086-983-9
000783216 0247_ $$2doi$$a10.2514/6.2008-2948
000783216 0247_ $$2SCOPUS$$aSCOPUS:2-s2.0-78249262340
000783216 0247_ $$2ISBN$$a9781563479397
000783216 037__ $$aRWTH-2020-02371
000783216 041__ $$aEnglish
000783216 1001_ $$aBui, Thanh$$b0$$eCorresponding author$$urwth
000783216 1112_ $$a14. AIAA/CEAS Aeroacoustics Conference$$cVancouver, British Columbia$$g29th AIAA Aeroacoustics Conference$$wCanada
000783216 245__ $$aNumerical Applicability of Different Sound Source Formulations to Compute Combustion Noise Using Acoustic Perturbation Equations for Reacting Flows$$honline
000783216 260__ $$bAmerican Institute of Aeronautics and Astronautics Reston, Virigina$$c2008
000783216 29510 $$a14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) : [Proceedings]
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000783216 7001_ $$aIhme, Matthias$$b1
000783216 7001_ $$0P:(DE-82)IDM00270$$aMeinke, Matthias$$b2$$urwth
000783216 7001_ $$aSchroeder, Wolfgang$$b3$$urwth
000783216 7001_ $$aPitsch, Heinz$$b4
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000783216 9141_ $$y2008
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000783216 9201_ $$0I:(DE-82)415110_20140620$$k415110$$lLehrstuhl für Strömungslehre und Aerodynamisches Institut$$x0
000783216 961__ $$c2020-02-19T15:23:41.957342$$x2020-02-19T15:23:41.957342$$z2020-02-19
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