1993
DOI: 10.2514/3.49105
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Low Aspect Ratio Wing Code Validation Experiment

Abstract: A code validation experiment for transonic flow is described. The experimental geometry is a low aspect ratio wing, tested in a solid wall wind tunnel. Inflow conditions were measured far enough upstream of the model to allow simple specification. Experimental uncertainties are given for pressure, temperature, velocity, and position measurements, as well as bounds on model deflections and transition location. Cursory comparison with simple computational models provides a baseline of flow conditions that should… Show more

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Cited by 4 publications
(1 citation statement)
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“…Pressures in the test section were measured using electronically scanned pressure transducers (PSI ESP-32, ±15 psid) that were calibrated before each run against a reference pressure transducer (Datametrics Barocel) 18 . Flow temperature was measured by thermocouples in the settling chamber.…”
Section: Pressure and Temperature Instrumentsmentioning
confidence: 99%
“…Pressures in the test section were measured using electronically scanned pressure transducers (PSI ESP-32, ±15 psid) that were calibrated before each run against a reference pressure transducer (Datametrics Barocel) 18 . Flow temperature was measured by thermocouples in the settling chamber.…”
Section: Pressure and Temperature Instrumentsmentioning
confidence: 99%