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.
Analysis and testing of stability augmentation systems
1972-06-13
Report
No indication
English
Analysis and Testing of Stability Augmentation Systems
NTIS | 1972
|Design GEM stability augmentation systems
Engineering Index Backfile | 1963
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