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The effects of a highly cambered low-drag wing and of auxiliary flaps on the high-speed aerodynamic characteristics of a twin-engine pursuit airplane model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1944 |
| Description | Results are presented for tests of two wings, an NACA 230-series wing and a highly-cambered NACA 66-series wing on a twin-engine pursuit airplane. Auxiliary control flaps were tested in combinations with each wing. Data showing comparison of high-speed aerodynamic characteristics of the model when equipped with each wing, the effect of the auxiliary control flaps on aerodynamic characteristics, and elevator effectiveness for the model with the 66-series wing are presented. High-speed aerodynamic characteristics of the model were improved with the 66-series wing. |
| File Size | 19982827 |
| Page Count | 59 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092692 |
| Archival Resource Key | ark:/13960/t89g8vv9j |
| Language | English |
| Publisher Date | 1944-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Naca 66,2-416-66,2-616 - Char & Moments Low-drag - (wing Flaps, Aux Airfoils - Naca 66 - Char & Moments Low-drag (wing Flaps, Auxiliary) Wind Tunne Airfoils - Naca 23016-4412 - Char & Moments Wing Flaps, Auxiliary Pressure Distribution - Wings - Lockheed P-58 Mach Number Diving - Pull-outs - Lockheed P-58 Pressure Distribution - Airfoils - Naca 66 Airfoils - Naca 230- Char & Moments Wing Flaps, Auxiliary 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 |
