Experimental and Numerical Investigation of a Single Stage Low Speed Axial Compressor with Tandem-Stator focusing on the Variation of the Second Airfoil Relative Position

Research output: Contribution to book/Conference proceedings/Anthology/Report › Conference contribution › Contributed › peer-review

Contributors

Details

Original languageEnglish
Title of host publicationConference: Deutscher Luft- und Raumfahrtkongress
Publication statusPublished - Jan 2014
Peer-reviewedYes

Symposium

TitleDeutscher Luft- und Raumfahrtkongress 2014
Conference number
Duration16 - 18 September 2014
Location
CityAugsburg
CountryGermany

External IDs

ORCID /0000-0003-0900-8298/work/194824240