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Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1960 |
| Description | Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability |
| File Size | 8474825 |
| Page Count | 89 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650018341 |
| Archival Resource Key | ark:/13960/t04z01815 |
| Language | English |
| Publisher Date | 1960-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Characteristics Directional Stability Canard Longitudinal Stability Wing Tip 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 |