NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The use of optimization techniques to design controlled diffusion compressor bladingA 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.
Document ID
19820006221
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sanger, N. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-82763
E-1084
Report Number: NASA-TM-82763
Report Number: E-1084
Meeting Information
Meeting: Ann. Intern. Gas Turbine Conf.
Location: London
Start Date: April 18, 1982
End Date: April 22, 1982
Sponsors: ASME
Accession Number
82N14094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available