Numerical Investigation of a Two-Bladed Propeller Inflow at Yaw (2020)

First Author: Higgins R
Attributed to:  Modelling and Simulation of helicopters and tilt-rotors in Vortex Ring State funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/1.c035647

Publication URI: http://dx.doi.org/10.2514/1.c035647

Type: Journal Article/Review

Parent Publication: Journal of Aircraft

Issue: 2

ISSN: 1533-3868