Similar Items: The development of a preliminary design process for the conversion of micro gas-turbine engine to a turboshaft configuration
- Micro gas turbine performance evaluation
- Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
- The development of an air-jet burner for the high intensity combustion of pulverised coal for a gas turbine.
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Author: Van der Spuy, S. J.
- Simulating the performance of the 24 ft. installed MinWaterCSP axial flow fan
- Experimental and numerical analysis of axial flow fans
- Numerical investigation of the effect of scaling on the performance of large scale axial flow fans.
- Development and verification of a centrifugal compressor test bench for Micro Gas Turbines (MGTs)
- Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor.
- Development of a one-dimensional code for the initial design of a micro gas turbine compressor stage