Research Catalog

Title

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

Author

Bozak, Richard F.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2017.

Details

Additional Authors

NASA Glenn Research Center, issuing body.

Description

1 online resource (6 pages) : color illustrations.

Series Statement

NASA/TM ; 2017-219489

Uniform Title

NASA technical memorandum ; 2017-219489.

Subject

• Acoustic properties
• Aerodynamic characteristics
• Bypass ratio
• Noise reduction
• Rotors
• Turbofan engines

Note

• "May 2017."

Bibliography (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)

Call Number

GPO Internet NAS 1.15:2017-219489

OCLC

marcive992989283

Author

Bozak, Richard F., author.

Title

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

Publisher

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2017.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2017-219489

NASA technical memorandum ; 2017-219489.

Bibliography

Includes bibliographical references (page 2).

Connect to:

https://purl.fdlp.gov/GPO/gpo82411

Added Author

NASA Glenn Research Center, issuing body.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2017-219489