A Computational Framework for Helicopter Fuselage Drag Reduction Using Vortex Generators
International annual forum; 70th, American Helicopter Society ; 2014 ; Montreal, Canada
2014-01-01
16 pages
Includes bibliographical references and author index.
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
A Computational Framework for Helicopter Fuselage Drag Reduction Using Vortex Generators
Online Contents | 2016
|British Library Conference Proceedings | 2016
|Helicopter drag reduction by vortex generators
Online Contents | 2015
|Helicopter drag reduction by vortex generators
Elsevier | 2015
|