Application of a Beamforming Technique to the Measurement of Airfoil Leading Edge Noise
Figure 10
Three-dimensional third-octave band sound maps, PPS 12/2 turbulence grid, m/s ( = 548,000), CLEAN-SC beamforming algorithm, center frequency 2 kHz. (Note that all sound maps are scaled to the same maximum level measured for the reference airfoil.).
(a) Nonporous reference airfoil,
(b) Porous airfoil made of Needlona felt, = 130,200 Pa
(c) Porous airfoil made of Recemat, = 8,200 Pa
(d) Porous airfoil made of M-Pore Al 45 ppi, = 1,000 Pa s/m2