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Experimentally determined local flow properties and drag coefficients for a family of blunt bodies at mach numbers from 2.49 to 4.63
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Experimentally determined local flow properties and drag coefficients for family of blunt bodies at Mach numbers from 2.49 to 4.63 |
| File Size | 1881146 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670030271 |
| Archival Resource Key | ark:/13960/t55f3jz5x |
| Language | English |
| Publisher Date | 1967-10-01 |
| Access Restriction | Open |
| Subject Keyword | Drag Coefficient Flow Measurement Blunt Body Supersonic Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |