Design Parametric Study of a Compound Wing-in-Ground Effect. I: Aerodynamics Performance-Reference-Cited by-同舟云学术

Design Parametric Study of a Compound Wing-in-Ground Effect. I: Aerodynamics Performance

Published:2016-01 Issue:1 Volume:29 Page:04015022
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jamei Saeed¹,Maimun Adi²,Mansor Shuhaimi³,Azwadi Nor⁴,Priyanto Agoes⁵

Affiliation:

1. Dept. of Marine Engineering, Faculty of Engineering, Persian Gulf Univ., Boushehr, Islamic Republic of Iran; formerly, Marine Technology Centre, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia (UTM), Skudai 81310, Johor, Malaysia.

2. Professor, Marine Technology Centre, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia (UTM), Skudai 81310, Johor, Malaysia (corresponding author).

3. Associate Professor, Dept. of Aeronautical Engineering, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia (UTM), Skudai 81310, Johor, Malaysia.

4. Associate Professor, Dept. of Thermo-Fluids, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia (UTM), Skudai 81310, Johor, Malaysia.

5. Assistant Professor, Marine Technology Centre, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia (UTM), Skudai 81310, Johor, Malaysia.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000380

Reference32 articles.

1. Numerical investigation of airfoil in ground proximity;Abramowski T.;J. Theor. Appl. Mech.,2007

2. Ahmed M. R. (2004). “Flow over thick airfoils in ground effect—An investigation on the influence of camber.” Proc. 24th Int. Congress of the Aeronautical Sciences ICAS.

3. An investigation on the aerodynamics of a symmetrical airfoil in ground effect

4. Lift Augmentation of a Low-Aspect-Ratio Thick Wing in Ground Effect

5. An evaluation of RANS turbulence modelling for aerodynamic applications

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