Flow around a hemisphere-cylinder at high angle of attack and low Reynolds number. Part I: Experimental and numerical investigation-Reference-Cited by-同舟云学术

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Flow around a hemisphere-cylinder at high angle of attack and low Reynolds number. Part I: Experimental and numerical investigation

Published:2015-07 Issue: Volume:44 Page:77-87
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Le Clainche Soledad,Li Jingyun I.,Theofilis Vassilis,Soria Julio

Funder

Marie Curie

Spanish Ministry of Science and Innovation

Defense Science and Technology Organization of Australia

Multi-modal Australian ScienceS Imaging and Visualisation Environment (MASSIVE)

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference56 articles.

1. Koopman-mode decomposition of the cylinder wake;Bagheri;J. Fluid Mech.,2013

2. Three-dimensional Floquet stability analysis of the wake of a circular cylinder;Barkley;J. Fluid Mech.,1996

3. Three-dimensional numerical simulation of the wake flow of an afterbody at subsonic speeds;Bohorquez;Theor. Comput. Fluid Dyn.,2012

4. Stability and dynamics of the laminar wake past a slender blunt-based axisymmetric body;Bohorquez;J. Fluid Mech.,2011

5. Variants of dynamic mode decomposition: boundary condition, Koopman, and Fourier analyses;Chen;J. Nonlinear Sci.,2012

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