Accession Number : ADA137585

Title :   The Present Calculation Method of Adhering Layers on Aircraft Wings,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Bao,H

PDF Url : ADA137585

Report Date : 13 Jan 1984

Pagination or Media Count : 13

Descriptors :   *Turbulent boundary layer, Numerical methods and procedures, Comparison, Differential equations, Mathematical models, Integration, Three dimensional flow, Vortices, Viscosity, Wings, Aircraft, Translations, china

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE