Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility / Richard F. Bozak.
- Physical Description: 1 online resource (6 pages) : color illustrations.
- Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2017.
|Bibliography, etc. Note:||
Includes bibliographical references (page 2).
|Source of Description Note:||
Description based on online resource; title from PDF title page (NASA, viewed July 7, 2017).
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