Accession Number : ADA181217

Title :   Journal of China University of Science and Technology (Selected Articles),

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

PDF Url : ADA181217

Report Date : 18 May 1987

Pagination or Media Count : 34

Abstract : Contents: Effect of Nose Bluntness on Twin Wave Interference; Application of Finite Element Method to Transonic Airfoils - A Preliminary Steady Subcritical Calculation. (Chinese Translations; China)

Descriptors :   *TRANSONIC AIRFOILS, *AERODYNAMIC FORCES, *NOSE CONES, SHOCK WAVES, CHINA, CHINESE LANGUAGE, TRANSLATIONS, BLUNT BODIES, INTERFERENCE, FINITE ELEMENT ANALYSIS, BLAST WAVES, SUPERSONIC CHARACTERISTICS, FLOW FIELDS

Subject Categories : Fluid Mechanics
      Guided Missile Reentry Vehicles
      Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE