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Supersonic coaxial jet experiment for cfd code validation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carty, A. A. Drummond, J. P. Cutler, A. D. Doerner, S. E. Diskin, G. S. |
| Copyright Year | 1999 |
| Description | A supersonic coaxial jet facility has been designed to provide experimental data suitable for the validation of CFD codes used to analyze high-speed propulsion flows. The center jet is of a light gas and the coflow jet is of air, and the mixing layer between them is compressible. Various methods have been employed in characterizing the jet flow field, including schlieren visualization, pitot, total temperature and gas sampling probe surveying, and RELIEF velocimetry. A Navier-Stokes code has been used to calculate the nozzle flow field and the results compared to the experiment. |
| File Size | 1113653 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20040086859 |
| Archival Resource Key | ark:/13960/t1zd2vq3v |
| Language | English |
| Publisher Date | 1999-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Navier-stokes Equation Nozzle Flow Computational Fluid Dynamics Temperature Probes Supersonic Jet Flow Research Facilities Propulsion Velocity Measurement Design Analysis Mixing Layers Fluids Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
