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Large-scale wind-tunnel tests in ground effect of a 35 deg sweptback wing jet transport model equipped with blowing boundary-layer-control trailing- and leading-edge flaps
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1963 |
| Description | Wind tunnel test of ground effect of 35-deg swept- back wing jet transport equipped with boundary layer control, trailing & leading edge flaps |
| File Size | 2078636 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630006046 |
| Archival Resource Key | ark:/13960/t6g20qk37 |
| Language | English |
| Publisher Date | 1963-05-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Stability Test Trailing-edge Flap Jet Transport Sweptback Wing Boundary Layer Control 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 |