Loading...
Please wait, while we are loading the content...
Similar Documents
Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 deg
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Henderson, W. P. Huffman, J. K. |
| Copyright Year | 1974 |
| Description | An investigation has been conducted to determine the effects of configuration variables on the lateral-directional stability characteristics of a wing-fuselage configuration. The variables under study included variations in the location of a single center-line vertical tail and twin vertical tails, wing height, fuselage strakes, and horizontal tails. The study was conducted in the Langley high-speed 7-by 10-foot tunnel at a Mach number of 0.30, at angles of attack up to 44 deg and at sideslip angles of 0 deg and plus or minus 5 deg. |
| File Size | 4937323 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740023308 |
| Archival Resource Key | ark:/13960/t0cv98r7s |
| Language | English |
| Publisher Date | 1974-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Stability Directional Stability Subsonic Speed Body-wing Configurations Wind Tunnel Stability Tests Lateral Stability Aerodynamic Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
