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TECHNICAL PAPERS: Gas Turbines: Aircraft Engine

Preliminary Gas Turbine Design Using the Multidisciplinary Design System MOPEDS

[+] Author and Article Information
P. Jeschke, J. Kurzke, R. Schaber, C. Riegler

MTU Aero Engines GmbH, Dachauer Str. 665, 80995 Munich, Germany

J. Eng. Gas Turbines Power 126(2), 258-264 (Jun 07, 2004) (7 pages) doi:10.1115/1.1639009 History: Received December 01, 2001; Revised March 01, 2002; Online June 07, 2004
Copyright © 2004 by ASME
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References

Figures

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Input sheet window for modules
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General arrangement of an engine to be analyzed
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General arrangement before (longer engine length) and after optimization (shorter engine length)
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HPC radius ratio variation. Dependent variables are divided by the optimal values of Section 3.1.
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High spool speed variation at MCL. Dependent variables are divided by the optimal values of Section 3.1.
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HPC stage number variation. Dependent variables are divided by the optimal values of Section 3.1.

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