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Effects of wing vertical location on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1959 |
| Description | Effects of wing vertical location on stability and control of canard aircraft at supersonic speeds |
| File Size | 15342309 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630002675 |
| Archival Resource Key | ark:/13960/t6b32kw8w |
| Language | English |
| Publisher Date | 1959-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Control Supersonic Speed Wing Aerodynamics Aircraft Stability AND Control Body-wing Combination Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |