Abstract
The influence of background crossflow on the formation process of leading vortex ring in starting jet has been systematically investigated over the range of 1≤Rv≤6 and 0.7≤L/D≤6, where Rv is the ratio of jet velocity to crossflow velocity and L/D is the ratio of jet column length to diameter. Particular attention is being paid to the unique interaction between the leading vortex ring and the trailing vortex structures. In general, the background crossflow disrupts the normal formation process of leading vortex ring by either stopping its growth prematurely (Rv≥2) or preventing it from formation entirely (Rv<2). For Rv≥2, a new line, denoted as the optimal curve, is proposed with the formation number to illustrate the optimal application characteristics. The formation number diminishes with decreasing Rv. The mechanisms responsible for the clockwise (L/D>L/Dtran) and anticlockwise (L/D<L/Dtran) rotations of leading vortex ring have been further analyzed via kinematics and vortex dynamics. L/Dtran represents the L/D corresponding to the transition of leading vortex ring from anticlockwise rotation to clockwise rotation. As for the inability to produce a complete leading vortex ring at Rv<2, it is largely due to the fact that the crossflow weakens and directly inhibits the roll-up for the shear layer of starting jet on the windward side.
Original language | English |
---|---|
Article number | 109590 |
Journal | Aerospace Science and Technology |
Volume | 155 |
DOIs | |
Publication status | Published - Dec 2024 |
Keywords
- Crossflow
- Starting jet
- Vortex ring