Laser Doppler velocimetry investigation of swirler flowfields
Journal Article
·
· Journal of Propulsion and Power; (USA)
- Texas A M Univ., College Station (USA) Carnegie-Mellon Univ., Pittsburgh, PA (USA) Parker Hannifin Corp., Cleveland, OH (USA)
Detailed measurements of mean and turbulent velocity components and turbulent shear stress components have been made for jet flows of 20-, 40-, and 60-deg swirlers for 750 and 1500 mm H{sub 2}O supply air pressure conditions. When the mean velocity components are normalized based on the maximum axial velocity at the nozzle exit, there is a very close similarity between normalized profiles at different supply pressures for each swirler. The recirculation zone, which depends on the degree of swirl and the swirler geometry, is not well established near the nozzle exit for the case of high ratio of the inner to outer radius of the swirler and of low degree of swirl. This can create a serious deposition problem of fuel droplets onto the hub surface. Measurements of turbulent velocity components demonstrate that each jet can be considered to be close to local isotropic turbulence except at the nozzle exit, where the magnitudes and decay of the fluctuations depend strongly on flow direction. 14 refs.
- OSTI ID:
- 6889417
- Journal Information:
- Journal of Propulsion and Power; (USA), Journal Name: Journal of Propulsion and Power; (USA) Vol. 6; ISSN JPPOE; ISSN 0748-4658
- Country of Publication:
- United States
- Language:
- English
Similar Records
Influence of inlet conditions on the flowfield in a model gas turbine combustor
Transient predictions of lateral jet injection into typical isothermal combustor flowfields
A swirling jet under the influence of a coaxial flow
Conference
·
Fri May 01 00:00:00 EDT 1992
· Experimental Thermal and Fluid Science; (United States)
·
OSTI ID:7109549
Transient predictions of lateral jet injection into typical isothermal combustor flowfields
Conference
·
Mon Dec 31 23:00:00 EST 1984
· AIAA Pap.; (United States)
·
OSTI ID:5627225
A swirling jet under the influence of a coaxial flow
Journal Article
·
Mon Sep 15 00:00:00 EDT 2008
· Experimental Thermal and Fluid Science
·
OSTI ID:21116048
Related Subjects
33 ADVANCED PROPULSION SYSTEMS
330103 -- Internal Combustion Engines-- Turbine
330603* -- Vehicle Design Factors-- Engine System
ATOMIZATION
COMBUSTION CHAMBERS
DROPLETS
ENGINES
FLUID FLOW
FUEL INJECTION SYSTEMS
FUEL SYSTEMS
GAS LASERS
GAS TURBINE ENGINES
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
JETS
LASERS
MEASURING INSTRUMENTS
NOZZLES
PARTICLES
TRANSPORT THEORY
TURBULENT FLOW
VELOCIMETERS
VELOCITY
VORTEX FLOW
330103 -- Internal Combustion Engines-- Turbine
330603* -- Vehicle Design Factors-- Engine System
ATOMIZATION
COMBUSTION CHAMBERS
DROPLETS
ENGINES
FLUID FLOW
FUEL INJECTION SYSTEMS
FUEL SYSTEMS
GAS LASERS
GAS TURBINE ENGINES
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
JETS
LASERS
MEASURING INSTRUMENTS
NOZZLES
PARTICLES
TRANSPORT THEORY
TURBULENT FLOW
VELOCIMETERS
VELOCITY
VORTEX FLOW