Research Catalog

Title

Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / Christopher E. Hughes, John A. Gazzaniga.

Author

Hughes, Christopher E.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Langley Research Center, November 2013.

Details

Additional Authors

• NASA Glenn Research Center, issuing body.
• United States. National Aeronautics and Space Administration, sponsoring body.

Description

1 online resource (22 pages) : color illustrations.

Series Statement

NASA/TM ; 2013-216073

Uniform Title

NASA technical memorandum ; 2013-216073.

Subject

• Aircraft performance
• Bypass ratio
• Fan blades
• Fixed wings
• Low speed wind tunnels
• Noise reduction

Note

• Title from title screen (viewed July 9, 2014).
• "November 2013."

Bibliography (note)

• Includes bibliographical references (pages 5-6).

Funding (note)

• Sponsored by National Aeronautics and Space Administration

Call Number

GPO Internet NAS 1.15:2013-216073

OCLC

marcive883242288

Author

Hughes, Christopher E., author.

Title

Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / Christopher E. Hughes, John A. Gazzaniga.

Publisher

Cleveland, Ohio : National Aeronautics and Space Administration, Langley Research Center, November 2013.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2013-216073

NASA technical memorandum ; 2013-216073.

Bibliography

Includes bibliographical references (pages 5-6).

Funding

Sponsored by National Aeronautics and Space Administration WBS 561581.02.08.03.18.04

E-17121

Connect to:

https://purl.fdlp.gov/GPO/gpo50535

Added Author

NASA Glenn Research Center, issuing body.

United States. National Aeronautics and Space Administration, sponsoring body.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2013-216073