The various aspects of the SR-30 turbojet engine are discussed. The SR-30 is equipped with an inlet nozzle, radial compressor, counter-flow combustion chamber, turbine, and exhaust nozzle. Each component is instrumented with thermocouples and pressure gages to allow a complete thermodynamic evaluation. The SR-30 gas turbine is modeled by the Brayton cycle which employs air as the working fluid.
|Original language||English (US)|
|Number of pages||21|
|Journal||ASEE Annual Conference Proceedings|
|State||Published - 2003|
|Event||2003 ASEE Annual Conference and Exposition: Staying in Tune with Engineering Education - Nashville, TN, United States|
Duration: Jun 22 2003 → Jun 25 2003