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NASA NTRS ยท 19840041418

A slotted test section numerical model for interference assessment

Abstract

A numerical model of a slotted wind tunnel test section, intended for use with sparsely measured wall pressures in a wall interference assessment procedure, is described. The numerical model includes a discrete finite length wall slot representation and accounts for the nonlinear effects of the dynamic pressure of the slot outflow jet and of the low energy of slot inflow air. By using th numerical model in a wall interference prediction mode, it is demonstrated that accounting for slot discreteness is important in interpreting wall pressures measured between slots, and that accounting for finite slot length and nonlinear effects in the slot boundary condition can yield significant departures from the wall interference predicted using the classical linear homogeneous infinite-length wall representation.

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BibTeXRIS

Kemp, W. B., Jr.. 1984-01-01. A slotted test section numerical model for interference assessment. https://ntrs.nasa.gov/citations/19840041418

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