NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The performance of an annular vane swirlerIn connection with the desirability of optimizing the design of a gas turbine combustion chamber, there exists a need for a more complete understanding of the fluid dynamics of the flow in such chambers. In order to satisfy this need, experimental and theoretical research is being conducted with the objective to study two-dimensional axisymmetric geometries under low speed, nonreacting, turbulent, swirling flow conditions. The flow enters the test section and proceeds into a larger chamber. Inlet swirl vanes are adjustable to a variety of vane angles. The present investigation concentrates on the time-mean flow characteristics which are generated by the upstream annular swirler. The investigation makes use of a five-hole pitot probe technique. A theoretical analysis of swirl numbers associated with several idealized exit velocity profiles is included, and values of the ratio of maximum swirl velocity to maximum axial velocity at different swirl strengths are given for each case.
Document ID
19830055122
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lilley, D. G.
(Oklahoma State University Stillwater, OK, United States)
Sander, G. F.
(Oklahoma State Univ. Stillwater, OK, United States)
Date Acquired
August 11, 2013
Publication Date
June 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 83-1326
Accession Number
83A36340
Funding Number(s)
CONTRACT_GRANT: NAS3-74
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available