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Numerical Applicability of Different Sound Source Formulations to Compute Combustion Noise Using Acoustic Perturbation Equations for Reacting Flows
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In
14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference) : [Proceedings]
2008
: American Institute of Aeronautics and Astronautics Reston, Virigina
Online
DOI: 10.2514/6.2008-2948
Einrichtungen
Dokumenttyp
Contribution to a book/Contribution to a conference proceedings
Format
online
Sprache
English
Anmerkung
Peer reviewed article
Externe Identnummern
SCOPUS: SCOPUS:2-s2.0-78249262340
Interne Identnummern
RWTH-2020-02371
Datensatz-ID: 783216
Beteiligte Länder
Germany, USA
Related:
Journal Article/Contribution to a book/Contribution to a conference proceedings
Numerical applicability of different sound source formulations to compute combustion noise using acoustic perturbation equations for reacting flows
14. Aeroacoustics Conference, AIAA/CEAS, Vancouver, British ColumbiaVancouver, British Columbia, Canada, 5 May 2008 - 7 May 2008
29. Aeroacoustics Conference, AIAA, Meeting location,
AIAA meeting papers on disc [13.]2008(5), (2008) special issue: "14th AIAA/CEAS Aeroacoustics Conference : (29th AIAA Aeroacoustics Conference) ; 5 - 7 May 2008, Vancouver, British Columbia, Canada ; [papers]" (978-1-563-47939-7)
inactive 2020-03-24
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