An Experimental Study of Loss Sources in a Fan Operating With Continuous Inlet Stagnation Pressure Distortion (2013)

First Author: Gunn E
Attributed to:  Fan system for a boundary layer ingesting jet engine funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1115/1.4007835

Publication URI: http://dx.doi.org/10.1115/1.4007835

Type: Journal Article/Review

Parent Publication: Journal of Turbomachinery

Issue: 5