Accession Number : ADA182577

Title :   China Aerodynamics Research Society.

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Report Date : 10 APR 1987

Pagination or Media Count : 242

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.

Descriptors :   *AERODYNAMIC CHARACTERISTICS, *AIRFOILS, CHINA, COMBUSTORS, CURVATURE, TUBES, FOREIGN TECHNOLOGY, LAMINAR FLOW, BODIES OF REVOLUTION, AERODYNAMICS, SOCIETIES, FLOW FIELDS, RECIRCULATION, DRAG REDUCTION, INCOMPRESSIBLE FLOW, POTENTIAL FLOW, NUMERICAL METHODS AND PROCEDURES, CONTROL, PASSIVE SYSTEMS, REENTRY VEHICLES, NOZZLES, SLENDER BODIES, TWO DIMENSIONAL, TRANSONIC AIRFOILS, FLUIDS, INCOMPRESSIBILITY, VISCOSITY, MATHEMATICAL MODELS, RECOVERY, SHOCK WAVES, ACOUSTIC VELOCITY, TRANSONIC FLOW, VISCOUS FLOW

Subject Categories : Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE