Airfoil optimization by the method of inverse boundary-value problems (Q1185625)
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: Airfoil optimization by the method of inverse boundary-value problems |
scientific article; zbMATH DE number 35684
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Airfoil optimization by the method of inverse boundary-value problems |
scientific article; zbMATH DE number 35684 |
Statements
Airfoil optimization by the method of inverse boundary-value problems (English)
0 references
28 June 1992
0 references
Some variational problems on the shape of impermeable wing sections that ensure maximum lift, minimum drag, and maximum aerodynamic quality for a given perimeter and one fixed-angle trailing edge in a non-separating plane steady incompressible viscous flow at high Reynolds numbers are formulated and solved. Functionals are constructed whose minimization is equivalent to the optimization of those characteristics. The existence and uniqueness of extreme points is analyzed. Examples of optimized wing sections are given.
0 references
variational problems
0 references
impermeable wing
0 references
incompressible viscous flow
0 references
existence and uniqueness
0 references
