Research Catalog

Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods

Title
Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / Gregory P. Herrick.
Author
Herrick, Gregory Paul, 1972-
Publication
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2014.

Available Online

https://purl.fdlp.gov/GPO/gpo57922

Details

Additional Authors
NASA Glenn Research Center, issuing body.
Description
1 online resource (17 pages) : color illustrations.
Series Statement
NASA/TM ; 2014-218447
Uniform Title
NASA technical memorandum ; 2014-218447.
Subject
  • Turbomachinery
  • Flutter analysis
  • Inlet flow
  • Computational fluid dynamics
  • Aeroelasticity
Note
  • Title from title screen (viewed on June 3, 2015).
  • "December 2014."
  • "Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
Bibliography (note)
  • Includes bibliographical references (pages 15-17).
Call Number
GPO Internet NAS 1.15:2014-218447
OCLC
marcive910630220
Author
Herrick, Gregory Paul, 1972- author.
Title
Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / Gregory P. Herrick.
Publisher
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2014.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 2014-218447
NASA technical memorandum ; 2014-218447.
Bibliography
Includes bibliographical references (pages 15-17).
Connect to:
https://purl.fdlp.gov/GPO/gpo57922
Added Author
NASA Glenn Research Center, issuing body.
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:2014-218447
View in Legacy Catalog