An Advanced Spray Model for Application to the Prediction of Gas Turbine Combustor Flowfields

doi 10.1115/99-gt-299

Full Text

Abstract

Available in

Date

June 7, 1999

Authors

Anil K. Tolpadi

Suresh K. Aggarwal

Hukam C. Mongia

Publisher

American Society of Mechanical Engineers

Related search

Application of OVERFLOW to Hypersonic Perfect Gas Flowfields

English

Application of Turbulent Reacting Flow Analysis in Gas Turbine Combustor Development

JSME International Journal Series B

English

Numerical Correlation of Gas Turbine Combustor Ignition

English

Flow Analysis of High Pressure Catalytic Combustor for Gas Turbine

English

Thermo-Acoustic Velocity Coupling in a Swirl Stabilized Gas Turbine Model Combustor

Combustion and Flame

Energy Engineering

Fuel Technology

Chemical Engineering

Power Technology

English

Active Optimization of the Performance of a Gas-Turbine Combustor

Combustion Science and Technology

Energy Engineering

Fuel Technology

Chemical Engineering

Power Technology

English

The Lagrangian PDF Transport Method for Simulations of Gas Turbine Combustor Flows

English

Dynamic Simulation of the Gravel Bed Combustor-Gas Turbine System

English

Three Dimensional Performance Prediction of Advanced Swirl Vanes for Gas Turbine Airblast Atomizers

English