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The use of augmented rotor inflow to predict rotorcraft responses in hover and low-speed manoeuvres (2022)

First Author: Agarwal D

Attributed to: Novel Approach to Rotorcraft Simulation Fidelity Enhancement and Assessment funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1017/aer.2021.123

Publication URI: http://dx.doi.org/10.1017/aer.2021.123

Type: Journal Article/Review

Parent Publication: The Aeronautical Journal

Issue: 1301