Test in the Unitary Plan Wind Tunnel at NASA’s Ames Research acd16-0013-027-0

A collaborative effort between NASA and Boeing Research and Technology, this test in the Unitary Plan Wind Tunnel at NASA's Ames Research Center in California served to characterize the aerodynamic performance and stability and control characteristics of a Truss Braced Wing configuration using pressure sensitive paint, infrared thermography, model deformation measurements, flow visualization and surface static pressures.