NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Temperature distribution study in a cooled radial inflow turbine rotorA numerical study to determine the temperature distribution in the rotor of a radial inflow turbine is presented. The study is based on the use of the finite element method in the three dimensional heat conduction problem. Different cooling techniques with various coolant to primary mass flow ratios are investigated. The resulting temperature distribution in the rotor are presented for comparison.
Document ID
19760035789
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hamed, A. (Cincinnati Univ. OH, United States)
Baskharone, E. (Cincinnati Univ. OH, United States)
Tabakoff, W. (Cincinnati, University Cincinnati, Ohio, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-44
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 26, 1976
End Date: January 28, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A18755
Funding Number(s)
CONTRACT_GRANT: NAS2-7850
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available