Adjoint formulation of a steady multistage turbomachinery interface using automatic differentiation (Q1625651)
From MaRDI portal
| This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: Adjoint formulation of a steady multistage turbomachinery interface using automatic differentiation |
scientific article; zbMATH DE number 6986792
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Adjoint formulation of a steady multistage turbomachinery interface using automatic differentiation |
scientific article; zbMATH DE number 6986792 |
Statements
Adjoint formulation of a steady multistage turbomachinery interface using automatic differentiation (English)
0 references
29 November 2018
0 references
discrete adjoint
0 references
mixing-plane
0 references
algorithmic differentiation
0 references
sensitivity analysis
0 references
shape optimization
0 references
endwall contouring
0 references
operating conditions
0 references
0 references