Morphing of a supercritical wing by means of trailing edge deformation and vibration at high Reynolds numbers: Experimental and numerical investigation-Reference-Cited by-同舟云学术

Morphing of a supercritical wing by means of trailing edge deformation and vibration at high Reynolds numbers: Experimental and numerical investigation

Published:2019-11 Issue: Volume:91 Page:102676
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Simiriotis N.,Jodin G.,Marouf A.,Elyakime P.^ORCID,Hoarau Y.,Hunt J.C.R.,Rouchon J.F.,Braza M.

Funder

European Commission

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference28 articles.

1. A review of morphing aircraft;Barbarino;J. Intell. Mater. Syst. Struct.,2011

2. The proper orthogonal decomposition in the analysis of turbulent flows;Berkooz;Annu. Rev. Fluid Mech.,1993

3. Anisotropic organised eddy simulation for the prediction of non-equilibrium turbulent flows around bodies;Bourguet;J. Fluids Struct.,2008

4. Successive stages and the role of natural vortex dislocations in three-dimensional wake transition;Braza;J. Fluid Mech.,2001

5. Turbulence properties in the cylinder wake at high Reynolds numbers;Braza;J. Fluids Struct.,2006

Cited by 28 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Study on Far-Field Noise Characteristic Generated by Wall-Mounted Swept Finite-Span Airfoil within Transonic Flow;Aerospace;2024-08-08

2. Morphing of high-lift wing-flap system with cambering and trailing-edge flapping at high Reynolds number towards a full airplane application;Journal of Fluids and Structures;2024-06

3. Aerodynamic design of a double slotted morphed flap airfoil– a numerical study;Frontiers in Mechanical Engineering;2024-03-15

4. Low-velocity impact response of the post-buckled FG-MEE plate resting on visco-Pasternak foundation: Magneto-electro-mechanical effects-based interaction analysis;Composite Structures;2024-03

5. Effect of realistic distributed loads on the bi-stable behavior of a pre-stressed aileron;Acta Mechanica;2024-02-28