Calculation of flow distribution in large radius ratio stages of axial flow turbines and comparison of theory and experiment
Abstract
A method of calculating stage parameters and flow distribution of axial turbines is described. The governing equations apply to space between the blade rows and are based on the assumption of rotationally symmetrical, compressible, adiabatic flow conditions. Results are presented for stage design and flow analysis calculations. Theoretical results from the calculation system are compared with experimental data from low pressure steam turbine tests.
- Publication:
-
Fluid Mechanics, Acoustics, and Design of Turbomachinery
- Pub Date:
- 1974
- Bibcode:
- 1974fmad.rept..565H
- Keywords:
-
- Adiabatic Flow;
- Axial Flow Turbines;
- Compressible Flow;
- Engine Design;
- Turbine Blades;
- Air Flow;
- Flow Characteristics;
- Flow Distribution;
- Pressure Gradients;
- Systems Analysis;
- Fluid Mechanics and Heat Transfer