Numerical analysis of the effect of vortex control mechanism on longitudinal aerodynamics of lifting body-Reference-Cited by-同舟云学术

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Numerical analysis of the effect of vortex control mechanism on longitudinal aerodynamics of lifting body

Published:2013-10 Issue:1 Volume:30 Page:232-238
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Badarudin Mohamad Badry Ahmad,Lee Yin-Jen,Chong Wen-Tong,Nik-Ghazali Nik-Nazri,Oon Cheen-Sean,Salim Newaz Kazi

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. The X-31 aircraft: advanced in aircraft agility and performance;Alcorn;Progress in Aerospace Sciences,1996

2. Unsteady flow phenomena associated with leading-edge vortices;Breitsamter;Progress in Aerospace Sciences,2008

3. The suppression of periodic vortex shedding from a rotating circular cylinder;Dol;Journal of Wind Engineering and Industrial Aerodynamics,2008

4. Fixed Wing Performance;Gallagher,1992

5. Control of a decelerating boundary layer, Part 1: Optimization of passive vortex generators;Godard;Aerospace Science and Technology,2006

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1. Experimental Study of a NACA0015 Circulation Control Airfoil Using Synthetic Jet Actuation;AIAA Journal;2021-09-28

2. Strategies for the applications of flow control downstream of a bluff body;Flow Measurement and Instrumentation;2017-03

3. A New Method to Optimize the Wake Flow of a Vehicle: The Leading Edge Rotating Cylinder;Mathematical Problems in Engineering;2017

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