NASA NTRS · 19870046340
Optimization and analysis of gas turbine engine blades
Abstract
A 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.
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Vandenbrink, D. J., Hopkins, D. A.. 1987-01-01. Optimization and analysis of gas turbine engine blades. https://ntrs.nasa.gov/citations/19870046340
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