Global stability analysis of an idealized compressor blade row. I. Single-blade passage analysis
A direct-adjoint mean flow global stability investigation of self-excited instabilities in an
idealized, two-dimensional compressor blade row at off-design conditions is carried out, with …
idealized, two-dimensional compressor blade row at off-design conditions is carried out, with …
Wavepackets Driving Trailing Edge Noise. Part II–Resolvent-Based Model
We present the results from a physics-based model of the trailing-edge (TE) noise radiated
by an airfoil, obtained from resolvent analysis of the turbulent mean flow. In our approach …
by an airfoil, obtained from resolvent analysis of the turbulent mean flow. In our approach …