The photoacoustic spectrum (PAS) of the host matrix is featureless in the wavelength range under consideration.
The host matrix shows no absorption in the wavelength range under consideration.
This is because in the Reynolds number range under consideration, the airfoil performance will drop regardless of the airfoil shape.
Although similar trends are quite evident, the experimentally observed average surface reflectance turns out to be much lower over the spectral range under consideration.
While there is strong sample-dependency on their pressure composition isotherms, all of them follow the Henry's Law in the pressure range under consideration.
However, in a propagation environment that is subject to intense shadowing (i.e., for large values of the [0, 12]-dB range under consideration), the classical Monte Carlo method fails at producing a representative set of sampled gains [24, 25].
While the lowest eigenfrequency of the original model is found at about 31 Hz, the corresponding value in the optimized variant exceeds 100 Hz being the upper bound of the frequency range under consideration.
It is seen from this figure that in the SNR range under consideration, the improvement in SNR in decidels is comparable for all the comparison methods, but they show comparatively lower values relative to the proposed method at all the levels of SNR.
