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Calculation by a finite difference method of supersonic turbulent boundary layers with tangential slot injection
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1971 |
| Description | Finite difference calculation based on eddy diffusivity and mixing length flow theory to characterize supersonic turbulent boundary layer with tangential slot injection |
| File Size | 3069463 |
| Page Count | 77 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710013093 |
| Archival Resource Key | ark:/13960/t3130mz0z |
| Language | English |
| Publisher Date | 1971-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |