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

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)

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Document Details

Document Type
Technical Report
Publication Date
May 18, 1987
Accession Number
ADA181217

Entities

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Airfoils
  • Blast
  • Blast Waves
  • Computers
  • Coordinate Systems
  • Equations
  • Experimental Data
  • Flow
  • Flow Fields
  • Fluid Flow
  • Foreign Technology
  • High Temperature
  • Mach Number
  • Pressure Distribution
  • Shock Waves
  • Steady Flow
  • Wave Interference

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Political Science/ International Relations/ European Studies