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A numerical simulation of a normal sonic jet into a hypersonic cross-flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chandra, Suresh Krishnamurthy, Ramesh Jeffries, Damon K. |
| Copyright Year | 1997 |
| Description | This study involves numerical modeling of a normal sonic jet injection into a hypersonic cross-flow. The numerical code used for simulation is GASP (General Aerodynamic Simulation Program.) First the numerical predictions are compared with well established solutions for compressible laminar flow. Then comparisons are made with non-injection test case measurements of surface pressure distributions. Good agreement with the measurements is observed. Currently comparisons are underway with the injection case. All the experimental data were generated at the Southampton University Light Piston Isentropic Compression Tube. |
| File Size | 212672 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20010000421 |
| Archival Resource Key | ark:/13960/t5t77bh9w |
| Language | English |
| Publisher Date | 1997-02-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Flat Plates Jet Flow Pressure Distribution Hypersonic Flow Mathematical Models Computerized Simulation Injection Nitrogen Cross Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
