Instability of a swept-wing boundary layer modulated by stationary flow perturbations
Journal article, 2013

A collection of illustrations of swept-wing boundary layer secondary instability at low subsonic flow velocities is presented in this paper. The experimental results, obtained by hot-wire "visualization," provide detailed insight into the spatio-temporal structure and evolution of oscillations in the three-dimensional laminar boundary layer disturbed by longitudinal vortices and streaky structures.

Author

Valery Chernoray

Chalmers, Applied Mechanics, Fluid Dynamics

A.V. Dovgal

G.R. Grek

V.V. Kozlov

Yury Litvinenko

Visualization of Mechanical Processes: An International Online Journal

2152-209X (eISSN)

Vol. 3 1

Subject Categories

Mechanical Engineering

Aerospace Engineering

Fluid Mechanics and Acoustics

Driving Forces

Sustainable development

Areas of Advance

Transport

Roots

Basic sciences

More information

Created

10/7/2017