Recent Advances in the Development of Combustor Design Tools
Author:
- 26 June 2003
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 15 references indexed in Scilit:
- TAPS: A Fourth Generation Propulsion Combustor Technology for Low Emissions2003
- Modeling of Gas Turbine Swirl Cup Dynamics, Part 5:Large Eddy Simulation of Cold Flow2003
- Establishment of a Confined Swirling Natural Gas/Air Flame as a Standard Flame: Temperature and Species Distributions from Laser Raman MeasurementsCombustion Science and Technology, 2002
- Experimental study of velocity flow field for a multiple swirl spray combustor2002
- Flow dynamics in a swirl combustorJournal of Turbulence, 2002
- Gas turbine combustor liner wall temperature calculation methodology2001
- Swirl cup modeling. I2001
- Dry Low Emissions Premixer CCD Modeling and Validation1998
- Combustor Design Criteria Validation. Volume II. Development Testing of Two Full-Scale Annular Gas Turbine Combustors1979
- An empirical/analytical design methodology for gas turbine combustors1978