Control moment characteristics of double-jet circulation control airfoil

被引：0

作者：

He Y. ^{[1
]}

Lei Y. ^{[2
]}

Zhang D. ^{[1
]}

Zhang Y. ^{[1
]}

Zhou Z. ^{[1
]}

机构：

[1] Aeronautics Engineering College, Air Force Engineering University, Xi'an

[2] Unit 95034 of the Chinese People's Liberation Army, Baise

来源：

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2021年 / 47卷 / 12期

关键词：

Aerodynamic characteristics; Circulation control; Numerical simulation; Rudderless aircraft; Steady jet;

D O I：

10.13700/j.bh.1001-5965.2021.0080

中图分类号：

学科分类号：

摘要：

In order to study the possibility of flight control by circulation control technology, the control moment characteristics of steady jet circulation control airfoil in steady flow field are studied. The aerodynamic coefficient variation rules of virtual rudder and traditional rudder produced by single jet and double jet are compared and analyzed by numerical simulation, and the aerodynamic moment control characteristics are verified based on the rudderless aircraft Circulation Control SCAOON (CCSCAOON). The verification results show that the virtual rudder under single jet can provide the rolling and pitching torque needed by aircraft, the action mechanism is similar, and the control performance is better than that of the traditional rudder. Whether under single jet or double jet, the aerodynamic characteristics of circulation control airfoils at high angle of attack are poor, which limits the use of circulation control angle of attack. The lift-drag ratio and control torque characteristics of double jet are better than those of single jet. By adjusting the momentum coefficient of the lower jet port, the virtual rudder under double jet can effectively reduce the coupling effect of yaw moment, rolling moment and pitching moment. © 2021, Editorial Board of JBUAA. All right reserved.

引用

页码：2641 / 2649

页数：8

共 29 条

[1] FU Z J, XU H Y, DU H, Et al., Investigation on flapless wing based on circulation control, Aeronautical Science and Technology, 31, 5, pp. 11-22, (2020)
[2] Key mechanical problems in new aircraft, pp. 88-94, (2018)
[3] ENGLAR R J., Circulation control for high lift and drag generation on STOL aircraft, Journal of Aircraft, 12, 5, pp. 457-463, (1975)
[4] JONES G S, JOSLIN R D., Applications of circulation control technology, (2006)
[5] ENGLAR R J., Circulation control for high lift and drag generation on STOL aircraft, Journal of Aircraft, 12, 5, pp. 457-463, (2015)
[6] ENGLAR R J., Circulation control pneumatic aerodynamics:Blown force and moment augmentation and modification-Past, present and future, Fluids 2000 Conference and Exhibit, (2000)
[7] FIELDING J, LAWSON C, MARTINS-PIRES R, Et al., Design, build and flight of the DEMON demonstrator UAV, 11th AIAA Aviation Technology, Integration and Operations (ATIO) Conference, (2011)
[8] FRITH S, WOOD N., Investigation of dual circulation control surfaces for flight control, 2nd AIAA Flow Control Conference, (2004)
[9] MILHOLEN W, JONES G, CHAN D., High-Reynolds number circulation control testing in the national transonic facility (invited), 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, (2012)
[10] JONES G S, MILHOLEN W E, CHAN D T, Et al., Development of the circulation control flow scheme used in the NTF semi-span FAST-MAC model, 31st AIAA Applied Aerodynamics Conference, (2013)

← 1 2 3 →