NASA Ames Unitary Plan Wind Tunnel

Aerodynamic Testing Infrastructure at NASA Ames

Located at NASA's Ames facility, the Unitary Plan Wind Tunnel serves as a cornerstone infrastructure supporting aeronautics and flight vehicle development. The facility provides specialized test planning and evaluation capabilities designed to analyze complex aerodynamic characteristics under controlled laboratory conditions.

Transonic and Supersonic Facility Capabilities

The facility features an 11×11-foot transonic test section alongside a 9×7-foot supersonic test section. These sections are supported by dedicated laboratories, including the Balance Calibration Lab and the Fluid Mechanics Lab, enabling precise measurements across critical velocity regimes.

Supporting Mission Evaluation and Aerodynamic Research

Integrated within the Aerosciences Evaluation and Test Capabilities (AETC) framework and connected with the National Full Scale Aerodynamic Complex, the wind tunnel supports comprehensive flow characterization. These evaluations remain essential for validating vehicle designs across both atmospheric and spaceflight development programs.