image of the Large-Scale Low-Boom (LSLB) Inlet in the 8- by 6-Foot Supersonic Wind Tunnel
image of the Large-Scale Low-Boom (LSLB) Inlet in the 8- by 6-Foot Supersonic Wind Tunnel
of NASA’s X-59 quiet supersonic aircraft was used in the project’s latest wind tunnel
of NASA’s X-59 quiet supersonic aircraft was used in the project’s latest wind tunnel
Curiosity Rover, tested in NASA’s Glenn Research Center 10- by 10-Foot Supersonic Wind Tunnel
Curiosity Rover, tested in NASA’s Glenn Research Center 10- by 10-Foot Supersonic Wind Tunnel
Inside NASA Ames‘ 9- by 7-Foot Supersonic Wind Tunnel, researcher Don Durston inspects
NASA Jan 06, 2016 Image Article Inside NASA Ames‘ 9- by 7-Foot Supersonic Wind Tunnel
Truss-Braced Wing aircraft is seen here installed for testing in the Unitary Plan Wind Tunnel – representing just half the airplane, sliced from nose to tail, is used so that the tunnel
Truss-Braced Wing aircraft, or TTBW, the concept design shown here inside a NASA wind tunnel
The dynamic stability of blunt bodies during planetary entry is difficult to quantify as computational methods have yet to demonstrate accurate predictive
coefficients more accurately than traditional ballistic range testing and wind tunnel
of an airfoil equipped with an anti-icing system, mounted in the Icing Research Tunnel
of an airfoil equipped with an anti-icing system, mounted in the Icing Research Tunnel
documenting CEV Parachute Assembly System (CPAS) Drogue Chute Testing at Texas A&M’s Wind Tunnel
documenting CEV Parachute Assembly System (CPAS) Drogue Chute Testing at Texas A&M’s Wind Tunnel
Anita Sengupta and Donn Liddle of NASA are pictured in the low speed wind tunnel
Anita Sengupta and Donn Liddle of NASA are pictured in the low speed wind tunnel
analyze data collected for the X-59’s flight control system through low-speed wind tunnel – Martin’s Skunk Works facility in Palmdale, California, completed low-speed wind tunnel – image, a technician works on the X-59 model during testing in the low-speed wind tunnel
analyze data collected for the X-59’s flight control system through low-speed wind tunnel
