TY - JOUR
T1 - Characterizing the performance of the SR-30 turbojet engine
AU - Witkowski, T.
AU - White, S.
AU - Dueñas, C. Ortiz
AU - Strykowski, Paul J
AU - Simon, Terrence W
N1 - Copyright:
Copyright 2012 Elsevier B.V., All rights reserved.
PY - 2003
Y1 - 2003
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=8744265114&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=8744265114&partnerID=8YFLogxK
M3 - Conference article
AN - SCOPUS:8744265114
SN - 0190-1052
SP - 7743
EP - 7763
JO - ASEE Annual Conference Proceedings
JF - ASEE Annual Conference Proceedings
T2 - 2003 ASEE Annual Conference and Exposition: Staying in Tune with Engineering Education
Y2 - 22 June 2003 through 25 June 2003
ER -