BOS and Hot-Film Analysis of a CH-53G Helicopter Wake in Ground Effect

Abstract

Constant temperature anemometry and background-oriented schlieren (BOS) measurements on a CH-53G helicopter (take off mass x 14t) are used to investigate the rotor wake including the vortex breakdown to statistical turbulence. Hovering flights at a range of hub heights O.50 < h < 0.83 were investigated. The position of the rotorcraft was optically tracked using markers affixed to the fuselage. A complete breakdown of the tip vortices was noted within 0.3fl of the rotor plane, in stark qualitative contrast to small scale experiments wich show the tip vortices persisting to the ground plane. The large (37m2) BOS field of view showed a small effect of vortex pairing and blade vortex interaction, which was overshadowed by the rapid wake breakdown. Vortex pairing was found to result from varying vortex convection velocities rather than from differences in the vortex spacing due to the blade track.