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Minimum drag of four versions of a swept-wing fighter airplane obtained from flight tests of rocket-boosted models at mach numbers from 0.81 to 1.71
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| File Size | 5284699 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930089399 |
| Archival Resource Key | ark:/13960/t1mh2bk9p |
| Language | English |
| Publisher Date | 1956-09-07 |
| 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 |