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Parametric (On-Design) Cycle Analysis for a Separate Exhaust Turbofan Engine with Interstage Turbine BurnerNo abstract available
Document ID
20150016158
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Liew, K. H. (Michigan Technological Univ. Houghton, MI, United States)
Urip, E. (Michigan Technological Univ. Houghton, MI, United States)
Yang, S. L. (Michigan Technological Univ. Houghton, MI, United States)
Siow, Y. K. (Michigan Technological Univ. Houghton, MI, United States)
Marek, C. J. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 19, 2015
Publication Date
October 4, 2004
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2005-213658/SUPP
E-15148
Report Number: NASA/TM-2005-213658/SUPP
Report Number: E-15148
Funding Number(s)
CONTRACT_GRANT: NAG3-2088
WBS: WBS 22-066-10-12
Distribution Limits
Public
Copyright
Public Use Permitted.

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