For many aerospace applications, the dominant airfoil self-noise source is Turbulent Boundary Layer Trailing Edge (TBL-TE) noise. The replacement of solid airfoil trailing edges with permeable materials proved to be an adequate noise reduction mean in previous studies. This thesis project contributes to the development of innovative permeable materials by assessing the feasibility of actively influencing their noise mitigation characteristics. The proposed activation mechanism consists of heating up a polymerically coated, porous trailing edge and thereby influencing the material geometry and seepage fluid properties. Heating of the polymeric coating layer led to slightly decreasing pore diameters due to thermal expansion. The main limitati...
This manuscript presents a numerical investigation of the turbulent boundary layer-trailing edge (TB...
Permeable trailing edges are experimentally investigated in this thesis as a mean tomitigate aeroaco...
The turbulent flow over a NACA 0018 airfoil with porous trailing edge inserts and the resulting scat...
The present work analyses broadband noise scattering from permeable trailing edges with identical mi...
The present work analyses broadband noise scattering from permeable trailing edges with identical mi...
Studies on porous trailing edges, manufactured with open-cell Ni-Cr-Al foams with sub-millimeter por...
Studies on porous trailing edges, manufactured with open-cell Ni-Cr-Al foams with sub-millimeter por...
Studies on porous trailing edges, manufactured with open-cell Ni-Cr-Al foams with sub-millimeter por...
This study focuses upon a new permeable topology design concept as an alternative to porous metal fo...
Permeable trailing edges are experimentally investigated in this thesis as a mean tomitigate aeroaco...
The present paper describes acoustic and hot–wire measurements that were done in the aeroacoustic wi...
This manuscript presents a numerical investigation of the turbulent boundary layer-trailing edge (TB...
The turbulent flow over a NACA 0018 airfoil with porous trailing edge inserts and the resulting scat...
Open-cell porous materials have been reported as a promising concept for mitigating turbulent bounda...
Open-cell porous materials have been reported as a promising concept for mitigating turbulent bounda...
This manuscript presents a numerical investigation of the turbulent boundary layer-trailing edge (TB...
Permeable trailing edges are experimentally investigated in this thesis as a mean tomitigate aeroaco...
The turbulent flow over a NACA 0018 airfoil with porous trailing edge inserts and the resulting scat...
The present work analyses broadband noise scattering from permeable trailing edges with identical mi...
The present work analyses broadband noise scattering from permeable trailing edges with identical mi...
Studies on porous trailing edges, manufactured with open-cell Ni-Cr-Al foams with sub-millimeter por...
Studies on porous trailing edges, manufactured with open-cell Ni-Cr-Al foams with sub-millimeter por...
Studies on porous trailing edges, manufactured with open-cell Ni-Cr-Al foams with sub-millimeter por...
This study focuses upon a new permeable topology design concept as an alternative to porous metal fo...
Permeable trailing edges are experimentally investigated in this thesis as a mean tomitigate aeroaco...
The present paper describes acoustic and hot–wire measurements that were done in the aeroacoustic wi...
This manuscript presents a numerical investigation of the turbulent boundary layer-trailing edge (TB...
The turbulent flow over a NACA 0018 airfoil with porous trailing edge inserts and the resulting scat...
Open-cell porous materials have been reported as a promising concept for mitigating turbulent bounda...
Open-cell porous materials have been reported as a promising concept for mitigating turbulent bounda...
This manuscript presents a numerical investigation of the turbulent boundary layer-trailing edge (TB...
Permeable trailing edges are experimentally investigated in this thesis as a mean tomitigate aeroaco...
The turbulent flow over a NACA 0018 airfoil with porous trailing edge inserts and the resulting scat...