The 14 by 22 Foot Subsonic Tunnel is an atmospheric, closed-return tunnel that provides the opportunity to test both powered and unpowered models of various fixed and rotary wing configurations.
Transonic Speed Regime
• Transonic Dynamics Tunnel (TDT)
• National Transonic Facility (NTF)
• 0.3 Meter Transonic Cryogenic Tunnel (0.3-M TCT) + Learn More
Supersonic Speed Regime
• 4-Foot Supersonic Unitary Plan Wind Tunnel (UPWT)
• 20-Inch Supersonic Wind Tunnel (SWT) + Learn More
Hypersonic Speed Regime
• Langley Aerothermodynamics Laboratory (LAL)
• 8-Foot High Temperature Tunnel (8’ HTT)
• Supersonic Combustion Ramjet Test Complex (SCRAMJET) + Learn More
Structures Testing • Combined Loads Test System (COLTS)
• Landing and Impact Research Facility (LandIR)
• Aircraft Landing Dynamics Facility (ALDF) + Learn More
Advanced Sensing and Optical Measurement Branch Research Areas
Learn more about the measurement techniques employed within the GFTD facilities + Visit Site