The simultaneous use of sophisticated servocontrols and electric flight control systems in modern combat aircraft has led to revisions in the classical standards governing the selection of structural design loads. New guidelines for the determination of design loads are suggested and their application is discussed with reference to structural design optimization techniques, flight mechanics, structural weight and aircraft flight characteristics.
Determination des Charges de Dimensionnement des Avions de Combat Actuels (Determination of Design Loads for Modern Combat Aircraft)
1988
7 pages
Report
No indication
English
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