Fountain Flow Visualization in Quadrotor Wake Decreasing Rotor Thrust In-Ground Effect

被引:4
作者
Otsuka, Hikaru [1 ,4 ]
Kohno, Masayoshi [2 ]
Nagatani, Keiji [3 ]
机构
[1] Tohoku Univ, Dept Aerosp Engn, Sendai, Miyagi 9808579, Japan
[2] Tohoku Univ, Dept Robot Engn, Sendai, Miyagi 9808579, Japan
[3] Univ Tokyo, Sch Engn, Tokyo 1138656, Japan
[4] Kanazawa Univ, Inst Sci & Engn, Fac Frontier Engn, Kanazawa, Ishikawa 9201192, Japan
来源
JOURNAL OF AIRCRAFT | 2024年 / 61卷 / 03期
基金
日本学术振兴会;
关键词
Rotorcrafts; Quadrotor; PIV; Thrust; Rotor Wake; Flow Visualization; Ground Effect; Multirotor;
D O I
10.2514/1.C037101
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Wake visualizations and thrust measurements of a quadrotor model were conducted to clarify the relationship between thrust and wake flow structure in-ground effects. The adjacent rotor distance, rotor height above ground, and the presence of a plate representing a generic quadrotor centerbody were varied. Thrust decreased when lowering the quadrotor to the ground when the adjacent rotor distance was over 2.2 times the rotor radius. Laser light sheet flow visualization showed quadrotor wake flow structures. Furthermore, visualization using particle image velocimetry showed an averaged vector map of wakes and fountain flow at the center of the quadrotor wake, which caused circulation with rotor passing flow and decreased rotor thrust. The center plate increased the sum of the rotor thrust and plate lift; however, circulation flow formed under the plate and caused the rotor thrust to decrease the in-ground effect. The results clarified that fountain flow development decreased the quadrotor thrust in-ground effect. Reducing the adjacent rotor distance weakened the development of fountain flow in the quadrotor wake and eliminated the decrease in rotor thrust near the ground.
引用
收藏
页码:761 / 773
页数:13
相关论文
共 23 条
[1]  
Betz A., 1937, NACA TM 836
[2]  
Caradonna F. X., 1980, 6 EUR ROT POW LIFT A
[3]  
Cheeseman I. C., 1955, AERONAUTICS RES COUN
[4]  
Conyers SA, 2018, IEEE INT CONF ROBOT, P1244
[5]  
Curtiss H., 1984, J AM HELICOPTER SOC, V29, P48, DOI [DOI 10.4050/JAHS.29.48, 10.4050/jahs.29.48]
[6]   Quasi-Steady In-Ground-Effect Model for Single and Multirotor Aerial Vehicles [J].
He, Xiang ;
Leang, Kam K. .
AIAA JOURNAL, 2020, 58 (12) :5318-5331
[7]   Numerical method for predicting IGE hover performance of a lifting rotor [J].
Itoga, N ;
Nagashima, T ;
Yoshizawa, Y ;
Prasad, JVR .
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2000, 43 (141) :122-129
[8]  
Johnson W., 1994, HELICOPTER THEORY, P122
[9]   A Review of Rotor Wake Physics and Modeling [J].
Komerath, Narayanan M. ;
Smith, Marilyn J. ;
Tung, Chee .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2011, 56 (02)
[10]  
Koo J., 1966, NAL T 113