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Development and flight evaluation of active controls in the l-1011. [including wing load alleviation and stability augmentation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Urie, D. M. Johnston, J. F. |
| Copyright Year | 1978 |
| Description | Active controls in the Lockheed L-1011 for increased energy efficiency are discussed. Active wing load alleviation for extended span, increased aspect ratio, and active stability augmentation with a smaller tail for reduced drag and weight are among the topics considered. Flight tests of active wing load alleviation on the baseline aircraft and moving-base piloted simulation developing criteria for stability augmentation are described. |
| File Size | 1958664 |
| Page Count | 39 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780021108 |
| Archival Resource Key | ark:/13960/t07x16131 |
| Language | English |
| Publisher Date | 1978-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests L-1011 Aircraft Drag Reduction Energy Conservation Weight Reduction Aircraft Design Aerodynamic Stability Wing Loading Aerodynamic Loads Aircraft Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
