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Ultra High Bypass Ratio Turbofan model in the 9-by 15-Foot Low Speed Wind Tunnel
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Ultra High Bypass Ratio Turbofan model in the 9-by 15-Foot Low Speed Wind Tunnel

Ultra High Bypass Integrated System Test Testing of an Ultra High Bypass Ratio Turbofan model in the 9-by 15-Foot Low Speed Wind Tunnel. Pratt & Whitney designed the experimental engine to meet new efficiency and noise reduction targets for commercial aircraft set by NASA and the Federal Aviation Administration. The 9-by 15 tests analyzed two noise reduction technologies.

Date
2015-07-01
Photographer / author
NASA/GRC/BRIDGET CASWELL
Collection
GRC
Archive
NASA Image and Video Library
Type
photograph

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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 Ratio Turbofan model in the 9-by 15-Foot Low Speed Wind Tunnel" (2015-07-01). NASA/GRC/NASA/GRC/BRIDGET CASWELL. Public domain. https://images.nasa.gov/details/GRC-2015-C-04209

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