
Test section of the 9- by 7-foot Unitary Plan Supersonic Wind Tunnel at NASA’s Ames Research Center, set up to…

Polystyrene Particles (PSL’s) being developed at NASA’s Langley Research Center for improved Particle Image Velocimetry Measurements

This mid-afternoon, 360-degree panorama was acquired by the Mast Camera (Mastcam) on NASA’s Curiosity Mars rover on April 4, 2016,…

Jet Exit Rig Balance: A flow-through force balance used to measure aerodynamic or propulsive forces/moments at NASA’s Glenn Research Center.

Jet Exit Rig Balance: A flow-through force balance used to measure aerodynamic or propulsive forces/moments at NASA’s Glenn Research Center.

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Close up of Jet Exit Rig Balance being worked on at NASA’s Glenn Research Center.

NTF Semi-Span Active Flow Control Calibration System at NASA’s Langley Research Center National Transonic Facility.

Balance Flexure Fillet Study research specimen being tested at NASA’s Langley Research Center.

New 30,000 lb normal force (lift) semi-span balance designed by NFMTC for NASA Ames Research Center’s 11-foot transonic wind tunnel…