A Boundary Element Method iterative procedure to compute the compressible response of an airfoil subjected to incoming turbulence

Leandro Dantas De Santana, Christophe F. Schram, W. Desmet

Research output: Contribution to conferencePaperpeer-review

2 Citations (Scopus)
Original languageEnglish
DOIs
Publication statusPublished - 2014
Externally publishedYes
Event20th AIAA/CEAS Aeroacoustics Conference 2014 - Atlanta, United States
Duration: 16 Jun 201420 Jun 2014
Conference number: 20

Conference

Conference20th AIAA/CEAS Aeroacoustics Conference 2014
CountryUnited States
CityAtlanta
Period16/06/1420/06/14

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