FLUTTER SUPPRESSION AND GUST ALLEVIATION USING ACTIVE CONTROLS - REVIEW OF DEVELOPMENTS AND APPLICATIONS BASED ON THE AERODYNAMIC ENERGY CONCEPT.

E. Nissim

פרסום מחקרי: תוצר מחקר מכנסהרצאהביקורת עמיתים

תקציר

The current state-of-the-art of the aerodynamic energy concept is reviewed. The latest applications of the relaxed energy concept, most of which are as yet unpublished, are also presented. These applications include the suppression of the external-store flutter of three different configurations of the YF-17 flutter model using a single trailing-edge (T. E. ) control surface activated by a single, fixed gain, control law. Also included are some initial results regarding the suppression of flutter of the 1/20 scale, low-speed wind-tunnel model of the Boeing 2707-300 supersonic transport, using an activated T. E. control surface.

שפה מקוריתאנגלית
עמודים600-615
מספר עמודים16
סטטוס פרסוםפורסם - 1978
אירועICAS (Int Counc of the Aeronaut Sci) Proc, 11th Congr - Lisbon, Port
משך הזמן: 10 ספט׳ 197816 ספט׳ 1978

כנס

כנסICAS (Int Counc of the Aeronaut Sci) Proc, 11th Congr
עירLisbon, Port
תקופה10/09/7816/09/78

טביעת אצבע

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