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A compendium of controlled diffusion blades generated by an automated inverse design procedureA set of sample cases was produced to test an automated design procedure developed at the NASA Lewis Research Center for the design of controlled diffusion blades. The range of application of the automated design procedure is documented. The results presented include characteristic compressor and turbine blade sections produced with the automated design code as well as various other airfoils produced with the base design method prior to the incorporation of the automated procedure.
Document ID
19890011625
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sanz, Jose M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-101968
NAS 1.15:101968
E-4665
Accession Number
89N20996
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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