Aeroelastic modelling and analyses of a short wing-propeller configuration

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Aeroelastic modelling and analyses of a short wing-propeller configuration

Rotorcraft designs with the ability to fly as an aircraft but take off and land vertically as helicopters were first introduced in the early 1950s. However, the development of such concept stopped after a few failed attempts. Similar configurations, in which wings are equipped with additional propul...

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Bibliographic Details
Main Author:	Wang, Zi
Format:	Thesis (University of Nottingham only)
Language:	English
Published:	2021
Subjects:	Aeroelasticity; Propellers Aerial; Rotors (Helicopters); Airplanes Wings
Online Access:	https://eprints.nottingham.ac.uk/65737/

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