The instability of an infinite swept attachment line boundary layer is considered in the linear regime. The basic three dimensional flow is shown to be susceptible to travelling wave disturbances which propagate along the attachment line. The effect of suction on the instability is discussed and the results suggest that the attachment line boundary layer on a swept wing can be significantly stabilized by extremely small amounts of suction. The results obtained are in excellent agreement with the available experimental observations
Crossflow instabilities dominate disturbance growth in the leading-edge region of swept wings. Strea...
A scheme for generating boundary layers is described and applied to an infinite swept wing model wit...
The discovery of a radial absolute instability mechanism on the boundary layer of a rotating disk1 m...
The 3-D boundary layer on a swept wing can support different types of hydrodynamic instability. Atte...
It is known that the incompressible, infinite swept attachment line flow is unstable to streamwise d...
The instability of a three dimensional attachment line boundary layer is considered in the nonlinear...
AbstractLaminar fiow in the boundary layer at the leading edge of swept airplane wings typically bec...
International audienceA formulation based on direct and adjoint parabolized equations is developed t...
We use numerical and asymptotic techniques to study the stability of a two-phase air/water flow abov...
Extensive combined experimental and theoretical investigations of the linear evolution of three-dime...
this paper. 5. Concluding remarks In this paper, the results of three-dimensional spatial direct num...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
The linear and the nonlinear stability of disturbances that propagate along the attach� ment line of...
A brief outline of the experimental and theoretical investigation of boundary layer instability mech...
The linear and the nonlinear stability of disturbances that propagate along the attachment line of a...
Crossflow instabilities dominate disturbance growth in the leading-edge region of swept wings. Strea...
A scheme for generating boundary layers is described and applied to an infinite swept wing model wit...
The discovery of a radial absolute instability mechanism on the boundary layer of a rotating disk1 m...
The 3-D boundary layer on a swept wing can support different types of hydrodynamic instability. Atte...
It is known that the incompressible, infinite swept attachment line flow is unstable to streamwise d...
The instability of a three dimensional attachment line boundary layer is considered in the nonlinear...
AbstractLaminar fiow in the boundary layer at the leading edge of swept airplane wings typically bec...
International audienceA formulation based on direct and adjoint parabolized equations is developed t...
We use numerical and asymptotic techniques to study the stability of a two-phase air/water flow abov...
Extensive combined experimental and theoretical investigations of the linear evolution of three-dime...
this paper. 5. Concluding remarks In this paper, the results of three-dimensional spatial direct num...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
The linear and the nonlinear stability of disturbances that propagate along the attach� ment line of...
A brief outline of the experimental and theoretical investigation of boundary layer instability mech...
The linear and the nonlinear stability of disturbances that propagate along the attachment line of a...
Crossflow instabilities dominate disturbance growth in the leading-edge region of swept wings. Strea...
A scheme for generating boundary layers is described and applied to an infinite swept wing model wit...
The discovery of a radial absolute instability mechanism on the boundary layer of a rotating disk1 m...