Parametric assessment of a folding wing-tip device for aircraft loads alleviation
Main Author: | Castrichini, Andrea |
---|---|
Published: |
University of Bristol
2017
|
Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720822 |
Similar Items
-
Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation
by: Agarwal, R K
Published: (2011) -
Design of Parametric Winglets and Wing tip devices : A Conceptual Design Approach
by: Rajendran, Saravanan
Published: (2012) -
Articulated blade tip devices for load alleviation on wind turbines
by: C. L. Bottasso, et al.
Published: (2016-12-01) -
Calculation of the Hinge Moments of a Folding Wing Aircraft during the Flight-Folding Process
by: Hao Xu, et al.
Published: (2019-01-01) -
Parametric Design of Aircraft Wing with Curved Leading Edge
by: Abdelkader BENAOULI, et al.
Published: (2018-03-01)