An experimental procedure for the determination of wake-airfoil interaction noise parameters

Leandro Dantas De Santana, Bence Toth, Christophe F. Schram

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

3 Citations (Scopus)
Original languageEnglish
Title of host publication19th AIAA/CEAS Aeroacoustics Conference
DOIs
Publication statusPublished - 2013
Externally publishedYes
Event19th AIAA/CEAS Aeroacoustics Conference, Aeroacoustics Conferences -
Duration: 27 May 201329 May 2013

Conference

Conference19th AIAA/CEAS Aeroacoustics Conference, Aeroacoustics Conferences
Period27/05/1329/05/13

Cite this

De Santana, Leandro Dantas ; Toth, Bence ; Schram, Christophe F. / An experimental procedure for the determination of wake-airfoil interaction noise parameters. 19th AIAA/CEAS Aeroacoustics Conference. 2013.
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title = "An experimental procedure for the determination of wake-airfoil interaction noise parameters",
author = "{De Santana}, {Leandro Dantas} and Bence Toth and Schram, {Christophe F.}",
year = "2013",
doi = "10.2514/6.2013-2060",
language = "English",
booktitle = "19th AIAA/CEAS Aeroacoustics Conference",

}

De Santana, LD, Toth, B & Schram, CF 2013, An experimental procedure for the determination of wake-airfoil interaction noise parameters. in 19th AIAA/CEAS Aeroacoustics Conference. 19th AIAA/CEAS Aeroacoustics Conference, Aeroacoustics Conferences, 27/05/13. https://doi.org/10.2514/6.2013-2060

An experimental procedure for the determination of wake-airfoil interaction noise parameters. / De Santana, Leandro Dantas; Toth, Bence; Schram, Christophe F.

19th AIAA/CEAS Aeroacoustics Conference. 2013.

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

TY - GEN

T1 - An experimental procedure for the determination of wake-airfoil interaction noise parameters

AU - De Santana, Leandro Dantas

AU - Toth, Bence

AU - Schram, Christophe F.

PY - 2013

Y1 - 2013

U2 - 10.2514/6.2013-2060

DO - 10.2514/6.2013-2060

M3 - Conference contribution

BT - 19th AIAA/CEAS Aeroacoustics Conference

ER -