Numerical Study of the Effect of Spoiler Configuration on Wake Vortex Alleviation-Reference-Cited by-同舟云学术

Numerical Study of the Effect of Spoiler Configuration on Wake Vortex Alleviation

Published:2015-05 Issue:3 Volume:28 Page:04014077
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ludin Hani B.¹,Omar Ashraf A.²,Asrar Waqar³

Affiliation:

1. Research Assistant, Dept. of Mechanical Engineering, International Islamic Univ. Malaysia, P.O. Box 10, 50728 Kuala Lumpur, Malaysia.

2. Professor, Dept. of Aeronautical Engineering, Univ. of Tripoli, P.O. Box 3601381, Tripoli, Libya.

3. Professor, Dept. of Mechanical Engineering, International Islamic Univ. Malaysia, P.O. Box 10, 50728 Kuala Lumpur, Malaysia (corresponding author).

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.1943-5525.0000406

Reference57 articles.

1. Barber M. R. and Tymczyszyn J. J. (1980). “Wake vortex attenuation flight tests: A status report.” NASA CP-2170 Washington DC.

2. Wake vortex characteristics of transport aircraft

3. On cooperative instabilities of parallel vortex pairs

4. CD-adapco. (2009). STAR-CCM+ User Guide Version 5.02 London.

5. Claude G. M. and John K. E. (2007). “Wake vortex alleviation using rapidly actuated segmented gurney flaps.” Flow Physics and Computation Division Stanford Univ. Stanford CA.

Cited by 2 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. Effect of a Directionally Porous Wing Tip on Tip Vortex;Journal of Applied Fluid Mechanics;2020-03-01

2. Influence of a Reverse Delta-Type Add-On Device on Wake Vortex Alleviation;AIAA Journal;2016-02