Full-Scale Tunnel (FST)
Purpose: To make possible wind tunnel research into areas that could be explored best with full-scale models or with actual aircraft.
Initial cost: $900,000
Circuit and pressure: Double-return, atmospheric
Test section: 30' x 60', open throat
Drive system: Two fans; two 4000-HP electric motors
Maximum speed: 118 MPH
Key members of design team: Smith J. DeFrance, Abraham Silverstein, Clinton H. Dearborn
Authorized: February 1929
Operational: 27 May 1931 (formally dedicated during the 6th Annual Aircraft Engineering Conference)
Major modifications: Equipped for free-flight dynamic model studies in 1960s. Underwent major rehabilitation in 1977.
Significance: "The FST is perhaps the best example of a major NACA facility that found a multitude of additional uses not visualized in the beginning. In 1962, for example, it had an extended study of the handling problems of hypersonic aircraft and space reentry vehicles like the shuttle, using large free-flying models." John V. Becker to author.
Disposition: Operational
Reference: TR 459
Construction of the Full-Scale Tunnel, 1930.
The P-51 Mustang is tested in the Full-Scale Tunnel, 1943.
In 1950 Langley tested the drag characteristics of what was then the world's fastest submarine, the Albacore, in the FST
Source:
appendix d