Acta Aerodynamics Sinica (Selected Articles),

Abstract

Contents: A Fast Algorithm of the Finite Difference Method for the Computation of the Transonic flow Past an Arbitrary Air foil with the Conservation of the Full Potential Equation; A Mixed Finite Difference Analysis of the Internal and External Transonic Flow Fields of Center Cone Inlet; Numerical Method for Viscous Shock-layer near the Stagnation Line of a Blunt Body; The Perfection and Application of the Flutter Subcritical Response Analysis; Calculation of Octagonal Wall Interference Factor Using Conformal Mapping; and Cryogenic High Reynolds Number Transonic Wind Tunnel with Pre-cooled and Restricted Flow.

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Document Details

Document Type
Technical Report
Publication Date
Nov 22, 1985
Accession Number
ADA162351

Entities

People

  • Huili Shen
  • Minggang Ji
  • Mingke Huang
  • Shijun Luo
  • Zongwen Xing

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Compressors
  • Difference Equations
  • Differential Equations
  • Flow Fields
  • Fluid Dynamics
  • Heat Transfer
  • High Pressure
  • Hypersonic Wind Tunnels
  • Inviscid Flow
  • Low Temperature
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Refrigeration Systems
  • Viscous Flow
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Dynamics.
  • Thin Film Deposition Science.