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Forces and moments on a yawed airfoil
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1939 |
| Description | The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing experiments with straight wings (zero dihedral), wings with dihedral, and wings with sweepback are evaluated within the range of sound angles of attack, explained by calculation and generally enlarged. |
| File Size | 962343 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930094510 |
| Archival Resource Key | ark:/13960/t6p01cc5x |
| Language | English |
| Publisher Date | 1939-01-01 |
| 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 |