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Maximum lift and longitudinal stability characteristics at reynolds numbers up to 7.8 x 10(exp 6) of a 35 degree sweptforward wing equipped with high-lift and stall-control devices, fuselage, and horizontal tail
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 4015836 |
| Page Count | 70 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085971 |
| Archival Resource Key | ark:/13960/t6tx7nx95 |
| Language | English |
| Publisher Date | 1950-02-09 |
| 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 |