X-56A ground vibration testing


Researchers at NASA Armstrong Flight Research Center have conducted ground vibration testing on the X-56A flex wing at the center’s Flight Loads Laboratory. Data collected from the impact testing includes fiber optic sensing system (FOSS) information, photogrammetry, flight accelerometers and ground vibration accelerometers.

The testing is important for studying wing characteristics before integration with the fuselage. The X-56A is crucial in testing high-aspect-ratio wings as an element in the design of future long-range aircraft.

Video of testing can be found here


About Author


With over 20 years experience in editorial management and content creation for multiple, market-leading titles at UKi Media & Events (publisher of Aerospace Testing International), one of the UK's fastest growing publishing companies, Anthony has written articles and news covering everything from aircraft, airports and cars, to cruise ships, trains, trucks and even tires!

Comments are closed.