Characterizing the performance of the SR-30 turbojet engine

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

Characterizing the performance of the SR-30 turbojet engine

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

Mechanical Engineering

Research output: Contribution to journal › Conference article › peer-review

25 Scopus citations

Abstract

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)
Pages (from-to)	7743-7763
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

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title = "Characterizing the performance of the SR-30 turbojet engine",

abstract = "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.",

author = "T. Witkowski and S. White and Due{\~n}as, \{C. Ortiz\} and Strykowski, \{Paul J\} and Simon, \{Terrence W\}",

note = "Copyright: Copyright 2012 Elsevier B.V., All rights reserved.; 2003 ASEE Annual Conference and Exposition: Staying in Tune with Engineering Education ; Conference date: 22-06-2003 Through 25-06-2003",

year = "2003",

language = "English (US)",

pages = "7743--7763",

journal = "ASEE Annual Conference Proceedings",

issn = "0190-1052",

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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

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 - https://www.scopus.com/pages/publications/8744265114

UR - https://www.scopus.com/pages/publications/8744265114#tab=citedBy

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 -

Characterizing the performance of the SR-30 turbojet engine

Abstract

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