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Benchmark Supercritical Wing on oscillating turntable at TDT

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Summary

View of semispan supercritical rectangular wing as tested on splitter plate at the Transonic Dynamics Tunnel. This model was oscillated at frequencies up to 30 hz to measure unsteady pressures due to pitch oscillations.

NASA Identifier: L2000-967

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nasa benchmark supercritical wing on oscillating turntable at tdt dvids experimental aircraft nasa history collection
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Date

10/12/2009
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Source

Defense Visual Information Distribution Service
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https://www.dvidshub.net/
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Public Domain Dedication. Public Use Notice of Limitations: https://www.dvidshub.net/about/copyright

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nasa benchmark supercritical wing on oscillating turntable at tdt dvids experimental aircraft nasa history collection