z-logo
open-access-imgOpen Access
Distributed Propulsion Aircraft with Aeroelastic Wing Shaping Control for Improved Aerodynamic Efficiency
Author(s) -
Nhan T. Nguyen,
Kevin Reynolds,
Eric B. Ting,
Natalia Nguyen
Publication year - 2018
Publication title -
journal of aircraft
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.64
H-Index - 94
eISSN - 1533-3868
pISSN - 0021-8669
DOI - 10.2514/1.c034448
Subject(s) - propulsion , aeroelasticity , wing , aerodynamics , aerospace engineering , engineering , wing twist , thrust , flutter , context (archaeology) , wing loading , aircraft flight mechanics , angle of attack , paleontology , biology
This study presents an aeroelastic wing shaping control concept for distributed propulsion aircraft. By leveraging wing flexibility, wing-mounted distributed propulsion can be used to re-twist wing...

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom