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 conference › Paper › peer-review

Original language	English
DOIs	https://doi.org/10.2514/6.2014-2323
Publication status	Published - 2014
Externally published	Yes
Event	20th AIAA/CEAS Aeroacoustics Conference 2014 - Atlanta, United States Duration: 16 Jun 2014 → 20 Jun 2014 Conference number: 20

Conference	20th AIAA/CEAS Aeroacoustics Conference 2014
Country/Territory	United States
City	Atlanta
Period	16/06/14 → 20/06/14

Access to Document

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

author = "{De Santana}, {Leandro Dantas} and Schram, {Christophe F.} and W. Desmet",

year = "2014",

doi = "10.2514/6.2014-2323",

language = "English",

note = "20th AIAA/CEAS Aeroacoustics Conference 2014 ; Conference date: 16-06-2014 Through 20-06-2014",

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TY - CONF

T1 - A Boundary Element Method iterative procedure to compute the compressible response of an airfoil subjected to incoming turbulence

AU - De Santana, Leandro Dantas

AU - Schram, Christophe F.

AU - Desmet, W.

N1 - Conference code: 20

PY - 2014

Y1 - 2014

U2 - 10.2514/6.2014-2323

DO - 10.2514/6.2014-2323

M3 - Paper

T2 - 20th AIAA/CEAS Aeroacoustics Conference 2014

Y2 - 16 June 2014 through 20 June 2014

ER -