NASA NTRS ยท 19790041933
Numerical spatial marching techniques in duct acoustics
Abstract
Direct calculation of the internal structure of a ducted noise source from farfield pressure measurements is regarded as an initial value problem, where the pressure and pressure gradient (farfield impedance) are assumed to be known along a line in the farfield. If pressure and impedance are known at the boundary of the farfield, the pressure can be uniquely determined in the vicinity of the inlet and inside the inlet ducting. A marching procedure is developed which, with this information obtained from measurements, enables a description of a ducted noise source. The technique uses a finite difference representation of the homogeneous Helmholtz equation.
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Baumeister, K. J.. 1979-02-01. Numerical spatial marching techniques in duct acoustics. https://ntrs.nasa.gov/citations/19790041933
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