DTIC ADA155480: Acta Aerodynamica Sinica pdf

DTIC ADA155480: Acta Aerodynamica Sinica

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Partial contents of this translation of Chinese reports: A boundary Element Technique in tRAnsonic Flow; EXploariotn of the Spatial Oscillation in Finite Difference Solutions for Navier-Stokes Shock; Calculation of Boundary Layer Growth behind an Unsteady Expansion WAve in A Tube; Numerical Computation for Insiscid Supersonic Flow Arough A Bent Cone; Theory of Similarity and the Profile of the Mean Density Distribution of Hypersonic Boundary Layer; The Engineering Numerical Technique for Determiniation of The Inviscid Flow Field Heating Rate on Ballistic Re-entry Vehicles; Vilsualization of Three Dimensional Separated Flows Using the Smoke Wire Technique: Application of Surface Hot Film in Aerodynamic Testing; and Measurement of the Coorelation between the Fluctuating Velocity in a Turbulent Boundary Layer

• Creator/s: Defense Technical Information Center
• Date: 4/30/1985
• Year: 1985
• Book Topics/Themes: DTIC Archive, , FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH, *BOUNDARY LAYER, *AERODYNAMICS, REENTRY VEHICLES, SPATIAL DISTRIBUTION, DENSITY, COMPUTATIONS, DISTRIBUTION, GROWTH(GENERAL), TEST METHODS, FINITE DIFFERENCE THEORY, SOLUTIONS(GENERAL), SHOCK, AERODYNAMIC CHARACTERISTICS, TRANSLATIONS, MEAN, SUPERSONIC FLOW, NAVIER STOKES EQUATIONS, OSCILLATION, INVISCID FLOW, FLOW SEPARATION, CHINA, BOUNDARY LAYER FLOW, HYPERSONIC FLOW, THREE DIMENSIONAL FLOW

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