NASA NTRS · 19920075365
The 40 X 80 X 120 Wind Tunnel Project
Abstract
The scope of this project includes increasing the speed of the 40 x 80 x 120 foot closed circuit wind tunnel to 300 knots to expand rotorcraft research capability, and to add an 80 x 120 foot open circuit wind tunnel with 100 knot maximum speed to expand vertical supersonic takeoff and landing research and capability. Topics discussed in viewgraph format are: wind tunnel characteristics, a cost analysis, and design of wind tunnel models.
Keep this discovery
Explore connections, maps & timelines
Falarski, Michael D.. 1984-03-20. The 40 X 80 X 120 Wind Tunnel Project. https://ntrs.nasa.gov/citations/19920075365
Cite the original work for its findings. Save a collection to share your selection of sources.