Accession Number : ADA118278

Title :   An Aerodynamic Design Method for Transonic Axial Flow Compressor Stage,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Zhu,Fang-Yuan ; Zhou,Xin-Hai

PDF Url : ADA118278

Report Date : 21 Jul 1982

Pagination or Media Count : 21

Descriptors :   *Transonic flow, *Three dimensional flow, *Flow fields, *Axial flow compressors, Axial flow compressor blades, Fan blades, Blade airfoils, Computer programs, Mathematical analysis, Translations, China

Subject Categories : Hydraulic and Pneumatic Equipment
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE