Drag decomposition of a subsonic wing via a far-field, exergy-based method (2022)
Attributed to:
Aero engine electrical fan performance for boundary layer ingestion applications
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1177/09544100221132649
Publication URI: http://dx.doi.org/10.1177/09544100221132649
Type: Journal Article/Review
Parent Publication: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Issue: 7