Cover Image

Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors /

Show other versions (1)
Bibliographic Details
Main Author: Brankovic, Andreja (Author)
Corporate Author: NASA Glenn Research Center
Format: Government Document eBook
Language:English
Published: Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2002.
Series:NASA technical memorandum ; 2002-211127.
Subjects:
Combustion chambers.
Lobe mixer.
Supersonic flow.
Pitot tubes.
Online Access:https://purl.fdlp.gov/GPO/LPS46077
Description
Item Description:"July 2002."
"Prepared for the 2001 19th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF 2001) cosponsored by IEEE, AES, NASA Glenn, and OAI, Cleveland, Ohio, August 27-30, 2001."
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
Physical Description:1 online resource (41 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 41).