INVESTIGATIONS OF NEAR WAKE FLOW FIELD AND HEAT TRANSFER ON TWO DIMENSIONAL AND AXIALLY SYMMETRIC BODIES AT SUPERSONIC SPEEDS
Abstract
Laminar and transitional heat transfer rates were measured in various base type separated flows in the shock tube. The application of the hot wire technique for measurements of the flow field in the supersonic near wake is studied. It is shown that using the measurements of a hot wire probe and a total pressure probe enable the determination of all the required physical parameters of the dissipative flow field in the near wake. The flow field behind a blunt two dimensional base model is measured. Mach number and total temperature profiles are determined and the various zones in the flow field are identified.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 30, 1969
- Accession Number
- AD0700115
Entities
People
- Josef Rom
Organizations
- Technion – Israel Institute of Technology