Accession Number : ADA131070

Title :   Solution of a Minimum Problem in Aircraft Wing Theory,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Nickel,Karl

PDF Url : ADA131070

Report Date : 19 Jul 1983

Pagination or Media Count : 14

Descriptors :   *Problem solving, *Wings, Lifting surfaces, Lift to drag ratio, Translations, East Germany

Subject Categories : Aircraft
      Numerical Mathematics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE