Accession Number:

ADA162993

Title:

Acta Aerodynanica Sinica (Selected Articles),

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Report Date:

1985-12-05

Pagination or Media Count:

182.0

Abstract:

Titles include Advances in the Study of Separated Flows Problems in Discrete Vortex Numerical Modelling of Vortex Motion behind a Circular Cylinder Calculation of Slender Delta Wing with Leading-edge Separation by Quasi-vortex-lattice Method Calculation of Flow around Thick Wing with Separation Vortices Split Coefficient Matrix Difference Method for Supersonic Three-dimensional Flow Some Characteristics of the FLIC Method and Its Application to Calculation of Pitot Pressure of Dusty-Gas Shock Tube Flow Experimental Investigation of Flap Turbulent Heat Transfer and Pressure Characteristics in Hypersonic Flow Laser Doppler Anemometer Measurements for Leading Edge Vortex Core Velocity of a Strake-wing Experimental Research of Boundary Layer Control Technique for Low Speed Multi-component Airfoils A Simpler Implicit Method to Solve N-S Equation Numerical Calculation of Separation Flow over Severely Indented Blunt Body Implicit Technique for Calculating Separated Base Flow Computation of Compressible Turbulent Separated Boundary Layer Inverse Boundary Layer Method for Separated Flow Wall Lift Interference Corrections in Ground Effect Testing. Translations China Chinese language

Subject Categories:

  • Numerical Mathematics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE