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Flow solution for advanced separate flow nozzles response a: structured grid navier-stokes approach
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kenzakowski, D. C. Shipman, J. Dash, S. M. |
| Copyright Year | 2001 |
| Description | NASA Glenn Research Center funded a computational study to investigate the effect of chevrons and tabs on the exhaust plume from separate flow nozzles. Numerical studies were conducted at typical takeoff power with 0.28 M flight speed. Report provides numerical data and insights into the mechanisms responsible for increased mixing. |
| File Size | 12045517 |
| Page Count | 67 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20010080469 |
| Archival Resource Key | ark:/13960/t13n73n2x |
| Language | English |
| Publisher Date | 2001-04-01 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Structured Grids Mathematics Noise Reduction Aircraft Noise Exhaust Gases Acoustic Nozzles Aeroacoustics Plumes Mixers Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
