A General Purpose Discrete Adjoint Formulation for Inviscid Flow Nozzle Design

2013 ◽  
Author(s):  
Andrea Dadone ◽  
Giovanni Caramia ◽  
Luciano Catalano
Keyword(s):  
Inviscid Flow ◽  
General Purpose ◽  
Nozzle Design ◽  
Discrete Adjoint ◽  
Adjoint Formulation

scholarly journals A Discrete Adjoint Formulation for Inviscid Flow Nozzle Optimization

2017 ◽  
Vol 126 ◽  
pp. 714-721
Author(s):  
Giovanni Caramia ◽  
Andrea Dadone
Keyword(s):  
Inviscid Flow ◽  
Discrete Adjoint ◽  
Adjoint Formulation

scholarly journals The Use of Optimization Techniques to Design Controlled Diffusion Compressor Blading

1982 ◽  
Author(s):  
N. L. Sanger
Keyword(s):  
Optimization Procedure ◽  
Inviscid Flow ◽  
General Purpose ◽  
Optimization Techniques ◽  
Conjugate Directions ◽  
Surface Boundary ◽  
Controlled Diffusion ◽  
Constrained Problems ◽  
Blade Section ◽  
Stator Blade

A method is presented for automating compressor blade design using numerical optimization, and is applied to the design of a controlled diffusion stator blade row. A general purpose optimization procedure is employed, which is 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 optimization concepts are briefly discussed. Selection of design objective and constraints is described. The procedure for automating the design of a two-dimensional blade section is discussed, and design results are presented.

Discrete Adjoint Formulation for Continuum Sensitivity Analysis

AIAA Journal ◽  
2016 ◽  
Vol 54 (2) ◽  
pp. 758-766 ◽  
Author(s):  
Mandar D. Kulkarni ◽  
David M. Cross ◽  
Robert A. Canfield
Keyword(s):  
Sensitivity Analysis ◽  
Discrete Adjoint ◽  
Adjoint Formulation ◽  
Continuum Sensitivity

scholarly journals The Use of Optimization Techniques to Design-Controlled Diffusion Compressor Blading

1983 ◽  
Vol 105 (2) ◽  
pp. 256-264 ◽  
Author(s):  
N. L. Sanger
Keyword(s):  
Optimization Procedure ◽  
Inviscid Flow ◽  
General Purpose ◽  
Optimization Techniques ◽  
Conjugate Directions ◽  
Surface Boundary ◽  
Controlled Diffusion ◽  
Constrained Problems ◽  
Blade Section ◽  
Stator Blade

A method is presented for automating compressor blade design using numerical optimization and is applied to the design of a controlled diffusion stator blade row. A general purpose optimization procedure is employed, which is 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 optimization concepts are briefly discussed. Selection of design of a two-dimensional blade section is discussed, and design results are presented.

Sign in / Sign up

Export Citation Format

Share Document