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Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at mach 10.5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1968 |
| Description | Integer relations method of determining inviscid shock layer flow and pressure distributions over blunt bodies |
| File Size | 884487 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19680006309 |
| Archival Resource Key | ark:/13960/t0ht7ck0j |
| Language | English |
| Publisher Date | 1968-02-01 |
| 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 |