Design of a swept wing wind tunnel model for study of cross-flow instability

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

Original languageEnglish
Title of host publicationProceedings of the 33rd AIAA applied aerodynamics conference
Editors s.n.
Place of PublicationReston
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages1-15
Number of pages15
ISBN (Print)978-1-62410-363-6
DOIs
Publication statusPublished - 2015
Event33rd AIAA applied aerodynamics conference, Dallas, USA - Reston
Duration: 22 Jun 201526 Jun 2015

Publication series

Name
PublisherAIAA

Conference

Conference33rd AIAA applied aerodynamics conference, Dallas, USA
Period22/06/1526/06/15

Cite this

Serpieri, J., & Kotsonis, M. (2015). Design of a swept wing wind tunnel model for study of cross-flow instability. In s.n. (Ed.), Proceedings of the 33rd AIAA applied aerodynamics conference (pp. 1-15). American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2015-2576