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Rolling, yawing, and hinge moments produced by rectangular ailerons
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1933 |
| Description | Ailerons described in references 1, 2, and 3, are summarized in the form of empirical equations which relate the aileron dimensions and displacements to the rolling, yawing, and hinge moments for pitch angles of 0 and 12 degrees, corresponding to angles of attack of the wings of 4 and 16 degrees, respectively. |
| File Size | 710180 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081199 |
| Archival Resource Key | ark:/13960/t8rc07p7v |
| Language | English |
| Publisher Date | 1933-01-01 |
| 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 |