Research Catalog

Title

The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / Christopher E. Hughes [and three others].

Author

Hughes, Christopher E.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.

Details

Additional Authors

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

Description

1 online resource (35 pages) : illustrations (some color).

Series Statement

NASA/TM ; 2013-214029

Uniform Title

NASA technical memorandum ; 2013-214029.

Subject

• Aeroacoustics
• Aerodynamic characteristics
• Aerodynamic noise
• Aircraft noise
• Fan blades
• Far fields
• Laser doppler velocimeters
• Low speed wind tunnels

Note

• Title from title screen (viewed July 9, 2014).
• "December 2013."
• "GT2005-68573."

Bibliography (note)

• Includes bibliographical references (page 13).

Funding (note)

• Sponsored by National Aeronautics and Space Administration

Call Number

GPO Internet NAS 1.15:2013-214029

OCLC

marcive883215359

Author

Hughes, Christopher E., author.

Title

The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / Christopher E. Hughes [and three others].

Publisher

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2013-214029

NASA technical memorandum ; 2013-214029.

Bibliography

Includes bibliographical references (page 13).

Funding

Sponsored by National Aeronautics and Space Administration WBS-22-781-30-75

E-15384

Connect to:

https://purl.fdlp.gov/GPO/gpo50531

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 1.15:2013-214029