Effect of rear-fuselage design on the aerodynamics of a helicopter at side-slip angle-Reference-Cited by-同舟云学术

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Effect of rear-fuselage design on the aerodynamics of a helicopter at side-slip angle

Published:2019-09 Issue: Volume:92 Page:192-197
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Gingras Drew,Weis Felix,Godbolt Bryan,Ghaemi Sina

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

1. Aerodynamic design optimisation for a helicopter configuration including a rotating rotor head;Breitsamter,2014

2. Wind-tunnel tests of a heavy-class helicopter optimised for drag reduction;Zanotti;Aeronaut. J.,2016

3. Helicopter fuselage drag reduction using active flow control: a comprehensive experimental investigation;Le Pape;J. Am. Helicopter Soc.,2015

4. A comprehensive PIV measurement campaign on a fully equipped helicopter model;De Gregorio;Exp. Fluids,2015

5. Aerodynamic analysis of a helicopter fuselage with rotating rotor head;Reß,2015

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical investigations on drag reduction of a civil light helicopter fuselage;Aerospace Science and Technology;2020-11

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