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.
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Details
NASA ID
GRC-2015-C-04209
Date Created
July 1, 2015
Center
GRC
Media Type
image
Photographer
NASA/GRC/BRIDGET CASWELL
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