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An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degrees sweepback : estimated downwash angles derived from pressure measurements on the tail at mach numbers of 1.40 and 1.59
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1952 |
| File Size | 12810463 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930087082 |
| Archival Resource Key | ark:/13960/t0xq1bm00 |
| Language | English |
| Publisher Date | 1952-03-10 |
| Access Restriction | Open |
| Subject Keyword | 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 |