Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility / Richard F. Bozak

Author: Bozak, Richard F.
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2017.
Physical Description: 1 online resource (6 pages) : color illustrations
Additional Creators: NASA Glenn Research Center

Access Online

purl.fdlp.gov

Availability

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Series

NASA technical memorandum ; 2017-219489

Restrictions on Access

Free-to-read Unrestricted online access

Report Numbers

NAS 1.15:2017-219489

Subject(s)

Acoustic properties
Aerodynamic characteristics
Bypass ratio
Noise reduction
Rotors
Turbofan engines

Note

"May 2017."

Bibliography Note

Includes bibliographical references (page 2).

Action Note

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View MARC record | catkey: 21046891