A comparison of the experimental and computational modelling of the fluidic turn-up vortex amplifier at full and zero swirl conditions

Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science

Volumn 215, Issue 8, 2001, Pages 893-904

  Woolhouse, R J ^a   Tippetts, J R ^a   Beck, S B M ^a  

^a UNIVERSITY OF SHEFFIELD   (United Kingdom)

Author keywords

Computational fluid dynamics; Fluidic; Gas turbine control; Vortex amplifier

Indexed keywords

COMBUSTORS; COMPUTER SIMULATION; DENSITY (SPECIFIC GRAVITY); GAS FUELS; REYNOLDS NUMBER; TURBULENCE; VORTEX FLOW;

REYNOLDS STRESS MODELS (RSM);

COMPUTATIONAL FLUID DYNAMICS;

CONTROL SYSTEM; FLUIDICS; GAS TURBINE;

EID: 0034764472     PISSN: 09544062     EISSN: None     Source Type: Journal    
DOI: 10.1243/0954406011524261     Document Type: Article

References (16)

1. The initial design of a fluidic variable geometry fuel injector for gas turbine combustion systems
2. Multi-switched vortex valves
3. Modulated swirl combustor
4. Mixture ratio control for the next generation of gas turbines
5. The use of fluidics in gas turbine combustion design
6. Versuche an der hydraulischen Ruckstromdrossel
7. Opposing control vortex valve
8. A filter blockage compensator circuit
9. Optimization of gas turbine combustor performance throughout the duty cycle
10. The interaction of the precessing vortex core and reverse flow zone in the exhaust of a swirl burner