NASA NTRS · 19840041401
Wall pressure measurements for three-dimensional transonic tests
Abstract
An experiment is described that provides input data for wind-tunnel wall interference assessment methods that are based on test-section wall pressure distributions. Wall pressures have been measured along orifice rows on the test-section walls during longitudinal force tests on two model sizes of the same configuration. These data were acquired at Mach numbers between 0.60 and 0.90 in a small, atmospheric transonic wind tunnel. A sample of the data and a discussion of results are presented.
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Sewall, W. G.. 1984-01-01. Wall pressure measurements for three-dimensional transonic tests. https://ntrs.nasa.gov/citations/19840041401
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