China Aerodynamics Research Society.

Abstract

Partial Contents: Airfoil Design at Sonic Velocity; The Passive Control of the Shock Waves on Transonic Airfoils; Computer-Aided Asymptotic Expansions of th Solution for Incompressible Potential Flow in Slender Two-Dimensional Nozzle; Numerical Modeling of Combustor Recirculation Flowfield; Multiple Laminar Flows of a Viscous, Incompressible Fluid Through a Curved Tube; An Improvement to the Numerical Method for Calculations of AIrcraft Configuration Longitudinal Aerodynamic Characteristics; Numerical Calculation of Swirling Flow in Combustor; Calculation of Transonic Viscous Flows Over an Arbitrary Airfoil; A Review of Aerodynamic Characteristics for Several Recovery Schemes of Reentry Vehicles; A Primary Investigation of Drag Reduction and Mechanism for a Blunt Body of Revolution with Slanted Base. Keywords: Foreign technology; China.

Document Details

Document Type
Technical Report
Publication Date
Apr 10, 1987
Accession Number
ADA182577

Entities

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Airfoils
  • Asymptotic Series
  • Blunt Bodies
  • Drag Reduction
  • Eddies (Fluid Mechanics)
  • Flow
  • Fluid Dynamics
  • Foreign Technology
  • Laminar Flow
  • Mechanical Properties
  • Potential Flow
  • Reentry Vehicles
  • Shock Waves
  • Transonic Airfoils
  • Two Dimensional
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.