Ultra High Bypass Integrated System Test
NASA’s Environmentally Responsible Aviation Project, in collaboration with the Federal Aviation Administration (FAA) and Pratt & Whitney, completed testing of an Ultra High Bypass Ratio Turbofan Model in the 9’ x 15’ Low Speed Wind Tunnel at NASA Glenn Research Center. The fan model is representative of the next generation of efficient and quiet Ultra High Bypass Ratio Turbofan Engine designs.
- Date
- 2015-09-14
- Collection
- GRC
- Archive
- NASA Image and Video Library
- Type
- photograph
Public domainsafest
Reason: a NASA work: not copyrighted in the United States.
Read from: NASA media usage guidelines: NASA material is not copyrighted in the US unless noted; no third-party credit or mark found.
Credit line
"Ultra High Bypass Integrated System Test" (2015-09-14). NASA/GRC. Public domain. https://images.nasa.gov/details/GRC-2015-C-04208Need photos for a whole script? Add Find Any Photo to Claude and ask for this one by its id: 90330.
More like this
Ultra High Bypass Ratio Turbofan model in the 9-by 15-Foot Low Speed Wind Tunnel
2015-07-01 · NASA Image and Video Library
Boundary Layer Ingestion
2016-12-15 · NASA Image and Video Library
Acoustic Casing Treatment Test
2017-02-14 · NASA Image and Video Library
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
2014-10-15 · NASA Image and Video Library
NASA Tests Advanced Air Mobility Aircraft Wing in Langley Wind Tunnel
2025-06-30 · NASA Image and Video Library
Vertical/Short Takeoff and Landing Model in the 10- by 10-Foot Supersonic Wind Tunnel
1979-05-23 · NASA Image and Video Library
GRC-2010-C-03457
2006-08-09 · NASA Image and Video Library
Pratt and Whitney J57 with a Greatex Nozzle in the Altitude Wind Tunnel
1957-02-23 · NASA Image and Video Library