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. (Author)
Analysis and Testing of Stability Augmentation Systems
1972
125 pages
Report
No indication
English
Analysis and testing of stability augmentation systems
NTRS | 1972
|Design GEM stability augmentation systems
Engineering Index Backfile | 1963
|