Zhang, T. and Barakos, G. N. (2019) Towards Optimisation of Compound Rotorcraft. In: 45th European Rotorcraft Forum, Warsaw, Poland, 17-20 Sep 2019,
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191617.pdf - Accepted Version 11MB |
Abstract
This work presents a tool-chain development for aerodynamic analysis and optimisation of compound rotorcraft. An automation framework for geometry composition and grid generation using ICEM Hexa is proposed, and variable applications are presented. High-fidelity CFD simulations of ducted fans are first performed to validate the in-house solver HMB3. Detailed analyses of the ducted fan and comparisons against experiments and simpler methods are presented, and good correlation can be noted. A compound helicopter model is then assembled, consisting of a parametrised Dauphin-like fuselage, ducted fans for auxiliary thrust, and a main rotor. Simulation methods of several fidelity levels using steady/unsteady actuator disks and resolved blades are conducted and evaluated. Analyses of the aerodynamics and flow features are then presented.
Item Type: | Conference Proceedings |
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Additional Information: | The sponsorship of the University of Glasgow and the China Scholarship Council is gratefully acknowledged. |
Status: | Published |
Refereed: | Yes |
Glasgow Author(s) Enlighten ID: | Barakos, Professor George and Zhang, Mr Tao |
Authors: | Zhang, T., and Barakos, G. N. |
Subjects: | T Technology > TL Motor vehicles. Aeronautics. Astronautics |
College/School: | College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity |
Research Group: | CFD Lab |
Copyright Holders: | Copyright © 2019 The Authors |
First Published: | First published in Proceedings of the 45th European Rotorcraft Forum |
Publisher Policy: | Reproduced in accordance with the publisher copyright policy |
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