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Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at mach numbers from 1.57 to 2.86
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1963 |
| Description | Afterbody geometry and sting diameter effect on aerodynamics of slender bodies at supersonic speed |
| File Size | 17531079 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19640000426 |
| Archival Resource Key | ark:/13960/t8cg4fm44 |
| Language | English |
| Publisher Date | 1963-11-01 |
| Access Restriction | Open |
| Subject Keyword | Slender Body Afterbody Aerodynamic Characteristics 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 |