Application of an Adaptive Shock Control Bump for Drag Reduction on a Variable Camber NLF Wing (AIAA 2018-0789)
Aerospace sciences meeting ; 2018 ; Kissimmee, FL
2018-01-01
15 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Variable Camber Compliant Wing - Design (AIAA 2015-1050)
British Library Conference Proceedings | 2015
|Efficient Active Rotor Concepts for In-Plane Noise Reduction (AIAA 2015-0789)
British Library Conference Proceedings | 2015
|