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The effect of inlet installation on the zero-lift drag of a 60 degree delta-wing--body configuration from flight tests at mach numbers from 0.8 to 1.86
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1955 |
| File Size | 14963231 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930088857 |
| Archival Resource Key | ark:/13960/t9n34kd9g |
| Language | English |
| Publisher Date | 1955-12-15 |
| 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 |