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Optimization and analysis of gas turbine engine bladesA gas turbine engine blade design is optimized using STAEBL. To validate the STAEBL analysis, the optimized blade design is analyzed using MARC, MHOST and BEST3D. The results show good agreement between STAEBL, MARC, and MHOST. The conclusion is that STAEBL can be used to optimize an engine blade design.
Document ID
19870046340
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vandenbrink, D. J. (Western Michigan University Kalamazoo, MI, United States)
Hopkins, D. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA PAPER 87-0827
Accession Number
87A33614
Distribution Limits
Public
Copyright
Other

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