Variable Density Tunnel

The Variable Density Tunnel is a wind tunnel at NASA Langley Research Center designed specifically for testing aircraft models. The steel tank measures approximately 34 feet long and 15 feet in diameter, housing all the equipment needed for aerodynamic research.

It was built in 1921 and introduced pressurized testing to American aeronautical research. This innovation allowed engineers to study aircraft designs under a range of conditions, leading to significant advances in flight technology.

The facility shaped how engineers thought about aircraft design during aviation's formative years. Visitors can sense this historical importance by seeing where groundbreaking aerodynamic work took place.

The tunnel is located on the NASA Langley Research Center grounds and can be viewed by visitors. It is worth checking ahead about access times and any security requirements, as it remains part of an active research facility.

The steel tank operated under extreme pressure conditions to create realistic testing scenarios for aircraft models. These high pressures allowed researchers to gather data that more accurately predicted how real aircraft would perform in flight.

Location: Virginia

Inception: 1921

Architects: Michael Max Munk

GPS coordinates: 37.07860,-76.34420

Latest update: December 12, 2025 12:08