Acta Aerodynamica Sinica,
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 30, 1985
- Accession Number
- ADA155480
Entities
Organizations
- National Air and Space Intelligence Center