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Using standard models provides beneficial data prior to customer tests in AEDC wind tunnels

This image shows the Sound Pressure Level distribution at 53.7 hertz frequency at Mach 0.8, Alpha 15 degrees on an AGARD-C model when using unsteady pressure sensitive paint during a test in the 16-foot transonic wind tunnel Dec. 3, 2021, at Arnold Air Force Base, Tenn. (U.S. Air Force image)

PHOTO BY: Jill Pickett
VIRIN: 220215-F-F3405-0001.PNG
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