The use of static or dynamic roughness elements has been shown in the past to delay the separation of a laminar boundary layer from a solid surface. Here, we examine analytically the effect of such elements on the local and breakaway separation points, corresponding respectively to the position of zero skin friction and presence of a singularity in the roughness region, for flow over a hump embedded within the boundary layer. Two types of roughness elements are studied: the first is small and placed near the point of vanishing skin friction; the second is larger and extends downstream. The forced flow solution is found as a sum of Fourier modes, reflecting the fixed frequency forcing of the dynamic roughness. Solutions for both the static a...
Over the last 60 years, there has been a great deal of research aimed at determining the impact of s...
Statistical and spectral analyses of the manipulation of a canonical zero pressure gradient turbulen...
Statistical and spectral analyses of the manipulation of a canonical zero pressure gradient turbulen...
The separation of a boundary layer from an aeroplane wing can have severe effects on aeroplane safet...
It has been shown experimentally that dynamic roughness elements – small bumps embedded within a bou...
The aircraft industry, as a whole, has been deeply concerned with improving the aerodynamic efficien...
Effects of roughness in boundary layers have to be addressed. Until adverse pressure gradient effect...
Separation of the turbulent boundary layer, is among the most critical phenomena that determine the ...
The study of transitional flows is considered crucial for many practical engineering applications. I...
The study of transitional flows is considered crucial for many practical engineering applications. I...
The study of transitional flows is considered crucial for many practical engineering applications. I...
The ever growing need in the aircraft industry to enhance the performance of a flight vehicle has le...
The ever growing need in the aircraft industry to enhance the performance of a flight vehicle has le...
The ever growing need in the aircraft industry to enhance the performance of a flight vehicle has le...
Computations are performed to study the flow past an isolated roughness element in a Mach 3.5, lamin...
Over the last 60 years, there has been a great deal of research aimed at determining the impact of s...
Statistical and spectral analyses of the manipulation of a canonical zero pressure gradient turbulen...
Statistical and spectral analyses of the manipulation of a canonical zero pressure gradient turbulen...
The separation of a boundary layer from an aeroplane wing can have severe effects on aeroplane safet...
It has been shown experimentally that dynamic roughness elements – small bumps embedded within a bou...
The aircraft industry, as a whole, has been deeply concerned with improving the aerodynamic efficien...
Effects of roughness in boundary layers have to be addressed. Until adverse pressure gradient effect...
Separation of the turbulent boundary layer, is among the most critical phenomena that determine the ...
The study of transitional flows is considered crucial for many practical engineering applications. I...
The study of transitional flows is considered crucial for many practical engineering applications. I...
The study of transitional flows is considered crucial for many practical engineering applications. I...
The ever growing need in the aircraft industry to enhance the performance of a flight vehicle has le...
The ever growing need in the aircraft industry to enhance the performance of a flight vehicle has le...
The ever growing need in the aircraft industry to enhance the performance of a flight vehicle has le...
Computations are performed to study the flow past an isolated roughness element in a Mach 3.5, lamin...
Over the last 60 years, there has been a great deal of research aimed at determining the impact of s...
Statistical and spectral analyses of the manipulation of a canonical zero pressure gradient turbulen...
Statistical and spectral analyses of the manipulation of a canonical zero pressure gradient turbulen...