Characterizing the performance of the SR-30 turbojet engine

T. Witkowski, S. White, C. Ortiz Dueñas, Paul J Strykowski, Terrence W Simon

Research output: Contribution to journalConference articlepeer-review

21 Scopus citations


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 languageEnglish (US)
Pages (from-to)7743-7763
Number of pages21
JournalASEE Annual Conference Proceedings
StatePublished - 2003
Event2003 ASEE Annual Conference and Exposition: Staying in Tune with Engineering Education - Nashville, TN, United States
Duration: Jun 22 2003Jun 25 2003


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