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Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 24583483 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082435 |
| Archival Resource Key | ark:/13960/t3rv4wh40 |
| Language | English |
| Publisher Date | 1948-11-01 |
| Access Restriction | Open |
| Subject Keyword | Wings, Tapered - Characteristics Airfoils - Naca 651-012 Low-drag Pressure Distribution - Ailerons Rolling, Pitching & Yawing Moments - Wings Ailerons, Sealed-gap Lateral Controls Devices Work Carried On At Lal Wind Tunnel Tests - Naca - 300 Mph (10'x 7') Work Carried On At Lal Ailerons - Hinge Moments 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 |