Abstract

Measurements of the evolution of wingtip trailing wake vortices in nonturbulent and unsheared density-stratified fluids are reported, using both laboratory experiments and a three-dimensional numerical code. As is widely known, and as our laboratory and numerical results confirm, the primary instability for these vortices in an unstratified fluid is the Crow instability, which has a characteristic initial wavelength of around 8.6b 0 , where b 0 is the initial separation distance between the vortices. In stratified fluids, however, our laboratory observations and numerical simulations show an instability with a shorter wavelength of around b 0 -2b 0 . This instability appears at a time in the evolution when the vertical migration of the vortices has reached nearly its maximum extent. The observed instability grows both in amplitude and wavelength with time. When the vortex Froude number is around one, the instability first becomes visible at a nondimensional time T of around 2 and reaches a maximum at T of around 4

Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call