NASA NTRS · 19900061906
Comparisons of one- and two- interface methods for tunnel wall interference calculation
Abstract
Tunnel wall interference in two-dimensional subsonic flow can be analytically calculated on the basis of the one- or two-interface method. The application of numerical integration by means of matrix multiplication to both methods has been found to significantly reduce CPU time in on-line operation. An investigation of the sensitivity of these methods to random velocity-measurement disturbances shows the one-interface method to be less sensitive to measurement errors, and therefore to be preferable for practical applications.
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Lo, C. F., Ulbrich, N.. 1990-08-01. Comparisons of one- and two- interface methods for tunnel wall interference calculation. https://ntrs.nasa.gov/citations/19900061906
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