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Analysis and testing of stability augmentation systems. [for supersonic transport aircraft wing and b-52 aircraft control system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sevart, F. D. Patel, S. M. Wattman, W. J. |
| Copyright Year | 1972 |
| Description | Testing and evaluation of stability augmentation systems for aircraft flight control were conducted. The flutter suppression system analysis of a scale supersonic transport wing model is described. Mechanization of the flutter suppression system is reported. The ride control synthesis for the B-52 aeroelastic model is discussed. Model analyses were conducted using equations of motion generated from generalized mass and stiffness data. |
| File Size | 4403787 |
| Page Count | 125 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740003696 |
| Archival Resource Key | ark:/13960/t0kt1fx7k |
| Language | English |
| Publisher Date | 1972-06-13 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Stability Systems Analysis Flutter Feedback Control Supersonic Transports Flight Control Aerodynamic Characteristics B-52 Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
