TY - JOUR
T1 - Numerical investigation into flow characteristics of tandem fan-wing configuration
AU - Shi, Zhenhai
AU - Yang, Weizhu
AU - Lu, Xiuru
AU - Yue, Zhufeng
N1 - Publisher Copyright:
© 2016, Press of Chinese Journal of Aeronautics. All right reserved.
PY - 2016/10/25
Y1 - 2016/10/25
N2 - Fan-wing can accelerate and rectify the air inflow through the rapid rotation of crow flow fan in the leading edge. Taking advantage of this distinguishing feature, a tandem fan-wing configuration is put forward, which is composed by double or multiple rows of fan-wings arranged in tandem with certain spacing and spatial distribution. The flow characteristics of the tandem fan-wing configuration are simulated based on two dimensional models, and the lift and thrust loads are calculated for different spacing, height disparities and row numbers. Results indicate that compared to single fan-wing, larger lift and thrust can be obtained by properly designed tandem fan-wing configuration. For instance, the four-row fan-wing with uniform spacing of one fan diameter possesses larger average lift and thrust by about 10% and 30%,respectively. The reason accounting for the improvement of lift and thrust is analyzed based on the flow filed near the fan-wings and the pressure distribution over the airfoils. These investigations can provide useful guidance for the design of future fan-wing aircraft with better low-speed large-load characteristics.
AB - Fan-wing can accelerate and rectify the air inflow through the rapid rotation of crow flow fan in the leading edge. Taking advantage of this distinguishing feature, a tandem fan-wing configuration is put forward, which is composed by double or multiple rows of fan-wings arranged in tandem with certain spacing and spatial distribution. The flow characteristics of the tandem fan-wing configuration are simulated based on two dimensional models, and the lift and thrust loads are calculated for different spacing, height disparities and row numbers. Results indicate that compared to single fan-wing, larger lift and thrust can be obtained by properly designed tandem fan-wing configuration. For instance, the four-row fan-wing with uniform spacing of one fan diameter possesses larger average lift and thrust by about 10% and 30%,respectively. The reason accounting for the improvement of lift and thrust is analyzed based on the flow filed near the fan-wings and the pressure distribution over the airfoils. These investigations can provide useful guidance for the design of future fan-wing aircraft with better low-speed large-load characteristics.
KW - Aerodynamic configuration
KW - Fan-wing
KW - Flow characteristics
KW - Row number
KW - Spacing
UR - http://www.scopus.com/inward/record.url?scp=84992486273&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2015.0356
DO - 10.7527/S1000-6893.2015.0356
M3 - 文章
AN - SCOPUS:84992486273
SN - 1000-6893
VL - 37
SP - 2922
EP - 2931
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 10
ER -