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    A compendium of controlled diffusion blades generated by an automated inverse design procedure (1989)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A 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.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-TM-101968 , E-4665 , NAS 1.15:101968
    Format: application/pdf
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