Ground boundary layers effect on aerodynamic coefficients of a compound wing with respect to design parameters-Reference-Cited by-同舟云学术

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Ground boundary layers effect on aerodynamic coefficients of a compound wing with respect to design parameters

Published:2018-09 Issue: Volume:164 Page:228-237
ISSN:0029-8018
Container-title:Ocean Engineering
language:en
Short-container-title:Ocean Engineering

Author:

Jamei Saeed,Maimun Adi,Azwadi Nor

Publisher

Elsevier BV

Subject

Ocean Engineering,Environmental Engineering

Reference22 articles.

1. Flow over thick airfoil in ground effect: an investigation on the influence of camber;Ahmed,2004

2. An investigation on the aerodynamics of a symmetrical airfoil in ground effect;Ahmed;J. Exp. Thermal 519 Fluid Sci.,2004

3. Aerodynamic of NACA4412 airfoil in ground effect;Ahmed;AIAA J.,2007

4. Aeronautic laboratory Universiti Teknologi Malaysia;ALUTM,2013

5. Wing in Ground Effect Craft Review;Halloran,1999

Cited by 5 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. Vortical flow characteristics of a slender delta wing in ground effect;Ocean Engineering;2022-10

2. Short-takeoff marine vehicle with circulation flow control of wing-in-ground effect;Ocean Engineering;2022-10

3. Numerical simulation of wake vortex for the flight near the ground with different boundary conditions;Engineering Applications of Computational Fluid Mechanics;2022-02-06

4. A development of longitudinal static stability analysis method of a Wing-In-Ground effect vehicle in cruise during the design process;Ocean Engineering;2022-01

5. Wake behind a Compound Wing in Ground Effect;Journal of Marine Science and Engineering;2020-03-01

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