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Feasibility Study for Low Drag Acoustic Liners Final ReportThis report documents the design and structural analysis as a final deliverable for the Phase 1 contract activity. Also included is a community noise test plan, which is a key deliverable for Phase 2. Finally, a high-level estimate (Phase 3 deliverable) is provided for the work statement of Phases 2-4, which covers the build of two inlet test articles, planning and execution of a flight test with the test inlets, as well as data analysis and final documentation. The two test inlets will be compared to the production baseline inlet configuration. There is also a plan to test one of the inlets "hardwalled" using speed tape or some other similar tape to block the acoustic perforations.
Document ID
20170007246
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Riedel, Brian
(Boeing Commercial Airplanes Propulsion Charleston, SC, United States)
Wu, Jackie
(Boeing Commercial Airplanes Propulsion Charleston, SC, United States)
Date Acquired
August 2, 2017
Publication Date
July 1, 2017
Subject Category
Acoustics
Report/Patent Number
NF1676L-27194
NASA/CR-2017-219648
Report Number: NF1676L-27194
Report Number: NASA/CR-2017-219648
Funding Number(s)
WBS: WBS 081876.02.07.03.01.01
CONTRACT_GRANT: NNL16AA04B
CONTRACT_GRANT: NNL16AB36T
Distribution Limits
Public
Copyright
Public Use Permitted.
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