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A rapid graphical method for computing the pressure distribution at supersonic speeds on a slender arbitrary body of revolution
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 1255011 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082441 |
| Archival Resource Key | ark:/13960/t2t481h5r |
| Language | English |
| Publisher Date | 1949-01-01 |
| Access Restriction | Open |
| Subject Keyword | Theories - Flow Supersonic Flow - Bodies Supersonic Pressure Distribution - Bodies 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 |