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A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| File Size | 992030 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082957 |
| Archival Resource Key | ark:/13960/t3mw6s17s |
| Language | English |
| Publisher Date | 1951-02-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils, Cambered Angle OF Attack Lift Distribution - Airfoils Airfoils - Naca 631 012 - Characteristics Theories - Airfoils, Thin Vortices - Airfoils Airfoils - Naca 64a810 (a=0 8) (mod ) - Characteristics Airfoils - Thickness Airfoils - Naca 0018 - Characteristics Airfoils - Naca 0010-63 (c1i=0 8) (mod ) (a=0 8) - Characteristics 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 |