1. Ocean College, Zhejiang University, Zhoushan 316021, China 2. The Engineering Research Center of Oceanic Sensing Technology and Equipment, Ministry of Education, Zhejiang University, Zhoushan 316021, China
A submarine manoeuvring turning test was conducted in a rotating arm basin at Zhejiang University by using the standard model SUBOFF AFF-8 as a test object in order to analyze the hydrodynamic characteristics and force motion of underwater vehicles in steady turn. The test technology of rotating arm test was introduced, including model installation, data measurement and calibration and verification of six component balance. The rotation derivatives of the horizontal and vertical planes were obtained and compared with the experimental values of the Taylor tank. Results showed that the error between Zhejiang University basin and Taylor tank was less than 10%, which proved the reliability of measurements for submarine maneuverability with Zhejiang University’s basin. The change curves of longitudinal force and transverse force with drift angle were symmetrical to the left and right with 0° drift angle as the dividing point when moving on the horizontal plane. The roll moment and yaw moment increased with the increase of drift angle. The vertical force and pitch moment were similar to parabola distribution with the change of drift angle. The forces and moments of the upward and downward movements were symmetrically distributed when moving on the vertical plane. The larger the angular velocity was, the larger the longitudinal force was. The force difference at different angles of attack was larger at higher angular velocities.
Bo-wen ZHAO,Ying-ying YUN,Ji-yuan SUN,Zhi-guo YANG,Bin HUANG. Study on rotating arm test of fully appended submarine and forces in single-plane. Journal of ZheJiang University (Engineering Science), 2023, 57(4): 773-783.
Fig.5Installation mode of strut, model and balance
Fig.6Horizontal inverted installation
Fig.7Installation form of vertical side mounting
Fig.8Calibration instrument of six-component balance
Fig.9Six loading conditions for calibrating coefficient matrix
Fig.10Verification results of coefficient matrix
Fig.11Force and moment on horizontal plane with radius of 16 m
Fig.12Dimensionless lateral force and yaw moment on horizontal plane
水池
$ {Y}_{{\rm{r}}}^{\mathrm{{'}}} $
$ {N}_{{\rm{r}}}^{\mathrm{{'}}} $
浙大水池
0.004 99
?0.004 08
泰勒水池
0.005 25
?0.004 44
误差/%
4.97
8.11
Tab.2Rotational derivatives of horizontal plane
Fig.13Dimensionless vertical force and pitch moment of upward floating on vertical plane
Fig.14Dimensionless vertical force and pitch moment of diving on vertical plane
垂直面
$ {Z}_{{\rm{q}}}^{\mathrm{{'}}} $
$ {M}_{{\rm{q}}}^{\mathrm{{'}}} $
浙大水池
泰勒水池
浙大水池
泰勒水池
上浮
?0.007 96
?0.007 55
?0.003 97
?0.003 7
下潜
?0.080 80
?0.007 55
?0.003 92
?0.003 7
Tab.3Rotational derivatives of vertical plane
Fig.15Repeat tests under condition of 0° drift angle on horizontal plane
ωr'
SDev/10?3
P(M)/10?3
?0.272
0.021
0.015 8
?0.311
0.154
0.116 0
?0.363
0.113
0.085 7
?0.436
0.169
0.128 0
Tab.4Standard deviation and precision limit of lateral force coefficient
Fig.16Variation curves of forces and moments with drift angles at different angular velocities on horizontal plane
Fig.17Variation curves of forces and moment with angles of attack at different angular velocities of vertical plane floating motion
Fig.18Variation curves of forces and moment with angles of attack at different angular velocities of vertical plane diving motion
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