Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1
Author:
Funder
National Natural Science Foundation of China
China Postdoctoral Science Foundation
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference26 articles.
1. Winglet multi-objective shape optimization;Elham;Aerosp. Sci. Technol.,2014
2. Mathematical model and stability analysis of fluttering and autorotation of an articulated plate into a flow;Rostami;Commun. Nonlinear Sci. Numer. Simul.,2018
3. Delayed detached Eddy simulation of wing flutter boundary using high order schemes;Gan;J. Fluids Struct.,2017
4. Flutter behavior of a flexible airfoil multiparameter experimental study;Gjerek;Aerosp. Sci. Technol.,2014
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