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Wind-tunnel investigation of a deflected- slipstream cruise-fan v/stol aircraft wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Wind tunnel tests of deflected slipstream cruise fan V/STOL aircraft wing |
| File Size | 3690737 |
| Page Count | 60 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19680001568 |
| Archival Resource Key | ark:/13960/t5jb0ws71 |
| Language | English |
| Publisher Date | 1967-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |