Acta Aerodynamica Sinica.

Abstract

CONTENTS: The Behavior of Separation Lines in a Steady Viscuous Flow Based on Analysis of Boundary Layer Equations; Numerical Prediction of Supersonic Boundary Layer Transition; An Iterative Method in Determining the Feedback Coefficients for the Multiloop Systems; The Movement of Hydrometeor Particle in a Bow Shock Layer; Numerical Calculations for Inviscous Transonic Flow Over Two-Dimensional Cascades; Kernel Function Method for Unsteady Transonic Flow Past Low-Frequency Oscillating Bodies of Revolution; Numerical Computation of Turbulent Jet Fields Using Two-Equation Turbulent Model; An Optimal Formulation of Simplified Three-Dimensional Navier Stokes Equations; Numerical Solution of Viscous Flows at Low Reynolds Number; Normal Force Characteristics of Sharp Nosed Bodies of Revolution at High Angles of Attack in Subsonic and Transonic Flow; Experimental Study on Turbulent Jet; A Method of Differentiating Interpolation Function in Solving Some Partial Differential Equations; Special Features of MacCormack's Scheme in Computing Unsteady Shock Wave; Applicability and Linkage of First-Order and Second-Order Shock-Expansion Methods; Improvement of Unsteady Aerodynamic Methods for lift Surface of Rotor Blades. (Chinese Translations)

Document Details

Document Type
Technical Report
Publication Date
Jan 06, 1987
Accession Number
ADA176552

Entities

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Bodies Of Revolution
  • Boundary Layer
  • Boundary Layer Transition
  • Bow Shock
  • Differential Equations
  • Equations
  • Flow
  • High Angles
  • Kernel Functions
  • Layers
  • Navier Stokes Equations
  • Partial Differential Equations
  • Reynolds Number
  • Shock
  • Shock Waves
  • Transonic Flow
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics