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Tests on an airfoil with two slots suitable for an aircraft of high performance : lift, drag, rolling and yawing moment measurements
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1926 |
| Description | The results that are described in this article form a complete series of tests on an airfoil fitted with front and rear slots, the rear slot being formed between the portion of the wing aft of the rear spar and the forward portion of the flap. |
| File Size | 8682216 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930090699 |
| Archival Resource Key | ark:/13960/t1xd42t4m |
| Language | English |
| Publisher Date | 1926-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils, Slotted Airfoils - Handley Page A 1 - Char , C P & Ordinates Airfoils - Handley Page A 1 Wing Slots - Char , Moments C P & Ordinates Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |