纵列式及横列式双旋翼流动的N-S方程模拟及气动特性的研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1999, Vol. 20 ›› Issue (6): 489-492.

• 论文 • Previous Articles Next Articles

STUDY OF THE AERODYNAMIC PROPERTIES OF TANDEM AND SIDE BY SIDE TWIN ROTOR CONFIGURATIONS BY NAVIER STOKES SIMULATION

TONG Zi-li, SUN Mao

Institute of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

Received:1998-08-24 Revised:1998-10-20 Online:1999-12-25 Published:1999-12-25

Abstract

Abstract: The 3 D incompressible N S equations with momentum source terms are solved to simulate the flow fields of tandem and side by side twin rotor configurations. Induced velocity distributions on rotor plane, aerodynamic properties and general flow fields of twin rotor configurations have been compared with those of single rotors, and the results reveal the aerodynamic interference between two rotors of the twin rotor.

Key words: tw in-ro to r, ro to r flow field, ro to r perfo rmance, N -S equat ions w ith momentum source term s

CLC Number:

V211. 3

TONG Zi-li;SUN Mao. STUDY OF THE AERODYNAMIC PROPERTIES OF TANDEM AND SIDE BY SIDE TWIN ROTOR CONFIGURATIONS BY NAVIER STOKES SIMULATION[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1999, 20(6): 489-492.

[1]	XIE Lijun, YANG Yunjun, LIU Zhou, ZHOU Weijiang. A high efficient method for computing dynamic derivatives of aircraft based on time spectral method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(6): 2016-2026.
[2]	REN Bi-ning;BAI Wen;ZHU Pei-ye;ZHOU Tian-xiao-. DEVELOPMENT OF AN OPEN CFD NUMERICAL SIMULATION SYSTEM [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1999, 20(6): 481-484.
[3]	Liu Yunlong;Liang Xingang;Qu Weilin;Ren Jianxun;Guo Zengyuan. GROUND THERMAL SCALE MODELING OF CONDUCTION CONVECTION RADIATION SYSTEMS IN MICRO GRAVITY ENVIRONMENT [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(6): 661-665.
[4]	Zhao Xiaohu;Yan Chao. AERODYNAMIC INVERSE DESIGN METHOD OF AIRFOIL VIA CFD [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(6): 648-651.
[5]	Kang Ning;Sun Mao. AERODYNAMIC FORCES AND BLADE FLAPPING MOTION OF A ROTOR IN FORWARD FLIGHT WITH GROUND EFFECTS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(6): 709-711.
[6]	Duan Zhanyuan;Tong Binggang;Jiang Guiqing. NEW WAY TO THE STUDY OF HIGH ORDER SCHEMES IN FEM [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(6): 716-719.
[7]	Hu Shuling;Liu Qiangang. GRID GENERATION AND EULER SOLVER FOR WING BODY TAIL CONFIGURATION [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(5): 531-534.
[8]	Xiao Li;Kuang Zhengqian;Kang Jichang. FRAME SYNCHRONIZATION AND COMMUNICATION STRATEGY IN AUTOMATIC PARALLELIZATION OF FLOWFIELD COMPUTATION [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(5): 523-526.
[9]	Cai Yuanhu;Zhang Kaiyuan;Mao Genwang. NUMERICAL SIMULATION FOR CHEMICAL NONEQUILIBRIUM FLOW [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(5): 515-518.
[10]	Luo Weiping;Wei Shengmin;Yang Pengji. DISTRIBUTED VIRTUAL WIND TUNNEL SYSTEM STRUCTURE AND WORKLOAD ANALYSIS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(5): 621-622.
[11]	Zhang Bo;Zhou Xingshe;Kang Jichang;Gu Jianhua. RESEARCH ON PVM PARALLEL PROGRAMMING DESIGN FOR FLOW FIELD COMPUTATION [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(3): 341-344.
[12]	Wang Qiang； Ma Handong； Wang Yiyun. A PARALLEL TRY FOR IMPLICIT FINITE DIFFERENCE ALGORITHM ON DISTRIBUTED MEMORY SYSTEMS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(3): 348-350.
[13]	Fan Zhaolin;Zhang Yulun;He Zhong. PRELIMINARY RESEARCH ON NUMERICAL SIMULATION OF TRANSONIC WALL INTERFERENCE FOR AIRCRAFT MODEL TESTS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(2): 210-214.
[14]	Qiao Zhide;Sun Gang;LiDong;Yang Shuchi. TRANSONIC NUMERICAL SIMULATION FORW ING-BODY-PYLON-NACELLE CONF IGURATION [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(2): 202-206.
[15]	Zhu Junzheng;Fan Xijun. GENERATION OF 3 D MUTLI BLOCKED STRUCTURE BODY FITTED GRIDS OF A COMPLEX CONFIGURATION FLYING BODY [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(1): 62-66.

STUDY OF THE AERODYNAMIC PROPERTIES OF TANDEM AND SIDE BY SIDE TWIN ROTOR CONFIGURATIONS BY NAVIER STOKES SIMULATION

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments