Experimental investigation of the effect of yaw angle on the inflow of a two-bladed propeller (2020)
Attributed to:
National Wind Tunnel Facility
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1016/j.ast.2020.105940
Publication URI: http://dx.doi.org/10.1016/j.ast.2020.105940
Type: Journal Article/Review
Parent Publication: Aerospace Science and Technology