NASA NTRS ยท 19820006221
The use of optimization techniques to design controlled diffusion compressor blading
Abstract
A method for automating compressor blade design using numerical optimization, and applied to the design of a controlled diffusion stator blade row is presented. A general purpose optimization procedure is employed, based on conjugate directions for locally unconstrained problems and on feasible directions for locally constrained problems. Coupled to the optimizer is an analysis package consisting of three analysis programs which calculate blade geometry, inviscid flow, and blade surface boundary layers. The optimizing concepts and selection of design objective and constraints are described. The procedure for automating the design of a two dimensional blade section is discussed, and design results are presented.
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Sanger, N. L.. 1982-01-01. The use of optimization techniques to design controlled diffusion compressor blading. https://ntrs.nasa.gov/citations/19820006221
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