Accession Number : AD0620105
Title : AN APPLICATION OF THE 'PLK-METHOD' TO CONFORMAL MAPPING AND THIN AIRFOIL THEORY.
Descriptive Note : Technical summary rept.,
Corporate Author : WISCONSIN UNIV MADISON MATHEMATICS RESEARCH CENTER
Personal Author(s) : Weissinger,J.
Report Date : MAY 1965
Pagination or Media Count : 27
Abstract : It is a widespread opinion that the 'PLK-Method' ('for rendering approximate solutions to physical problems uniformly valid') cannot be applied to problems of elliptic partial differential equations, especially not to thin airfoil theory. It is shown that this is not true-at least for symmetrical airfoils - if right use is made of the flexibility of the technique. An example shows that the technique can be used very successfully for numerical computations. (Author)
Descriptors : (*AIRFOILS, THEORY), (*CONFORMAL MAPPING, AIRFOILS), PARTIAL DIFFERENTIAL EQUATIONS, AERODYNAMIC CONFIGURATIONS, THIN WINGS, BOUNDARY VALUE PROBLEMS, ANGLE OF ATTACK
Distribution Statement : APPROVED FOR PUBLIC RELEASE