Numerical research on roll and sideslip coupling motions about a slender delta-wing

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 28, Issue 1, 2007, Pages 14-19

  Yang, Yun Jun ^a   Cui, Er Jie ^a   Zhou, Wei Jiang ^a  

^a CHINA ACADEMY OF AEROSPACE AERODYNAMICS   (China)

Author keywords

CFD; Coupling motion; Limit cycle; Sub iterative; Wing rock

Indexed keywords

BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; WINGS;

AEROCRAFT; LIMIT CYCLE; WING ROCK;

AIRCRAFT;

EID: 34249869331     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (10)

1. Yang Y J, Cui E J, Zhou W J. Effects of compressibility on the asymmetry development of vortex flow around a slender body[J]. Acta Aeronautica et Astronautica Sinica, 2004, 25(4): 333-338. (in Chinese)
2. Hall R M, Woodson S H. Introduction to the abrupt wing stall program[J]. Journal of Aircraft, 2004, 41(3): 425-435.
3. Nguyen L E, Yin L P, Chambers J R. Self-induced wing rock of slender delta wings[R]. AIAA 81-1883, 1981.
4. Yoshinaga T, Otaka S, Tate A. Wing rock of double wings[R]. AIAA 2001-4078, 2001.
5. Tang M Z, Wang T, Zhang W, et al. The roll experiment research on subsonic delta-wing[J]. Acta Aerodynamic Sinica, 1997, 15(4): 436-443. (in Chinese)
6. Yang X M, Cheng H M, Zhang Z G. Experiment and numerical simulation on wing rock of an 80-degree-swept flat-plate delta wing at high angle of attack[C]//Aerodynamics Research Memoirs. Beijing. 1994: 142-148. (in Chinese)
7. Kandil O A, Menzies M A. Effective control of computational simulated wing rock in subsonic flow[R]. AIAA 97-0831, 1997.
8. Gainer T G. A discrete-vortex method for studying the wing rock of delta wings[R]. NASA/TP-2002-211965, 2002.
9. Jun Y W, Nelson R C. Leading edge vortex dynamics on a delta wing undergoing a wing rock motion[R]. AIAA 87-0332, 1987.
10. Ericsson L E. Surprising developments in the search of analytic means for prediction of slender wing rock[R]. AIAA 2002-0712, 2002.