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High-lift and lateral control characteristics of an naca 652-215 semispan wing equipped with plug and retractable ailerons and a full-span slotted flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 2397735 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082548 |
| Archival Resource Key | ark:/13960/t3906g11d |
| Language | English |
| Publisher Date | 1949-04-01 |
| Access Restriction | Open |
| Subject Keyword | Ailerons, Retractable Wing Flaps, Slotted - Full-span Airfoils - Naca 65-210 - Low-drag Wind Tunnel Tests - Naca - 300-mph (10'x7') Airfoils - Naca 652-215 - Ordinates - Low-drag Lateral Control & High Lift - Work Carried On At Lal Wing Flaps, Slotted AND Ailerons Wings - Characteristics Rolling, Pitching & Yawing Moments - Wings Ailerons, Spoiler-slot - Plug 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 |