TY - GEN
T1 - Numerical simulation of water spray caused by a rolling airplane tire
AU - Qu, Qiulin
AU - Zhang, Fan
AU - Liu, Peiqing
AU - Agarwal, Ramesh K.
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2015
Y1 - 2015
N2 - The meshless method of smooth particle hydrodynamics (SPH) is used to simulate the water spray caused by a rolling airplane tire, which is a complex physical problem. Graphics of the spray at a certain tire speed are given to describe the whole process in detail. Flow field at different tire speeds demonstrate that as the tire speed increases, splashes as well as the scroll effect of the rolling movement become more pronounced. Furthermore, the angles between the runway and main jet flow fields at both sides increases. Results are also presented on splashes through different depths of the water film. The quantity of water over the tire decreases as the thickness of the water film increases. In this paper, for the first time in literature, detailed results of the whole water spray process are given and the effect of tire speed and pool depth on water spray is quantified.
AB - The meshless method of smooth particle hydrodynamics (SPH) is used to simulate the water spray caused by a rolling airplane tire, which is a complex physical problem. Graphics of the spray at a certain tire speed are given to describe the whole process in detail. Flow field at different tire speeds demonstrate that as the tire speed increases, splashes as well as the scroll effect of the rolling movement become more pronounced. Furthermore, the angles between the runway and main jet flow fields at both sides increases. Results are also presented on splashes through different depths of the water film. The quantity of water over the tire decreases as the thickness of the water film increases. In this paper, for the first time in literature, detailed results of the whole water spray process are given and the effect of tire speed and pool depth on water spray is quantified.
UR - http://www.scopus.com/inward/record.url?scp=85067319129&partnerID=8YFLogxK
U2 - 10.2514/6.2015-2413
DO - 10.2514/6.2015-2413
M3 - Conference contribution
AN - SCOPUS:85067319129
SN - 9781624103636
T3 - 33rd AIAA Applied Aerodynamics Conference
BT - 33rd AIAA Applied Aerodynamics Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 33rd AIAA Applied Aerodynamics Conference, 2015
Y2 - 22 June 2015 through 26 June 2015
ER -