@inproceedings{4c7c28495a4e4c5db4a5a735b9bb0f03,
title = "Effect of nose tip on wing rock of slender delta wing",
abstract = "The root cause of wing rock is investigated by examining two slender delta wings (70° and 85° sweep back angle) in wind tunnel using force measurement, pressure measurement and PIV techniques. The results show presence of asymmetric flow at 20° angle of attack and initiation of wing rock at the same point for 85° model while there is neither asymmetric flow nor wing rock for 70° model suggesting close relation of flow asymmetry with wing rock. Investigation with three apparently identical nose sections reveals that the asymmetry comes from the area very close to the wing tip. This asymmetric flow causes the vortices to interact in a complex way resulting in wing rock when the vortices are in close proximity (such as for 85° model), which is not the case when the vortices are 'comparatively away' (such as 70° model) from each other.",
keywords = "Asymmetric flow, Nose perturbation, Slender delta wing, Wing rock",
author = "Bakaul, \{Saifur Rahman\} and Yankui Wang and Guangxing Wu and Qureshi Humayun",
year = "2012",
doi = "10.4028/www.scientific.net/AMM.232.178",
language = "英语",
isbn = "9783037855140",
series = "Applied Mechanics and Materials",
pages = "178--183",
booktitle = "Mechanical and Aerospace Engineering",
note = "2012 3rd International Conference on Mechanical and Aerospace Engineering, ICMAE 2012 ; Conference date: 07-07-2012 Through 08-07-2012",
}