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NASA NTRS ยท 19820060711

Higher-order flow angle corrections for three-dimensional wind tunnel wall interference

Abstract

A second-order theory including camber effects in wind tunnel wall interference corrections is described. Changes in the geometrical configuration of the model tested are avoided by introducing the camber correction as an equivalent angle-of-attack correction. Tabular and graphic data are presented which indicate improved accuracy for second-order over first-order theory.

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BibTeXRIS

Rizk, M. H.. 1982-10-01. Higher-order flow angle corrections for three-dimensional wind tunnel wall interference. https://ntrs.nasa.gov/citations/19820060711

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