포텐셜 패널과 와류 조각 연계방법을 이용한 로터 공력 해석 Potential Panel and Vortex Particle Coupling Analysis

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 333
  • Download : 0
Rotor wake causes unsteady aerodynamics of rotor blade. So, accurate prediction of wake is very important and vortex method is good solution for this problem. Aerodynamic force of the rotor blade is calculated by potential panel method and the rotor wake is simulated by vortex particle method. The vortex particle method is easier to treat wake-body interaction and has better performance to expect the effect of ground and fuselage interaction. Rotor in hovering and forward flight condition is simulated through these methods. Thrust and surface pressure of rotor are compared with experiment data.
Publisher
한국군사과학기술학회
Issue Date
2013-08
Language
Korean
Citation

한국군사과학기술학회지, v.16, no.4, pp.481 - 485

ISSN
1598-9127
URI
http://hdl.handle.net/10203/201573
Appears in Collection
AE-Journal Papers(저널논문)
Files in This Item
There are no files associated with this item.

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0