Similar Items: Design methodology of an axial-flow turbine for a micro jet engine
- The development of an air-jet burner for the high intensity combustion of pulverised coal for a gas turbine.
- Micro gas turbine performance evaluation
- The development of a preliminary design process for the conversion of micro gas-turbine engine to a turboshaft configuration
- Design of a centrifugal compressor for application in micro gas turbines
- Performance evaluation of a micro gas turbine centrifugal compressor diffuser
- Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
Author: Von Backstrom, T. W.
- An evaluation of a scale model medium speed wind tunnel
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- Development of a low cost linear fresnel solar concentrator
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- Performance improvement of the Rover 1S/60 Gas Turbine Compressor
- The design of a low-noise rotor-only axial flow fan series