Titlebook: Structural Control; Proceedings of the S H. H. E. Leipholz Conference proceedings 1987 Springer Science+Business Media Dordrecht 1987 Optim

Tremor

Structural Control of Aircraft design stage such as controlling the wing resonant mode shapes. The aim is to avoid aeroelastic problems. Other modifications were found necessary to be introduced at service life, such as that needed to avoid the resulting acoustic fatigue failure of aircraft components in the vicinity of the jet

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GREEN

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某人

Structural Control of Aircraft meeting of the Acoustical Society of America at San Diego, California at 11 November 1983, respectively. This paper presents a method of structural control required to increase the load carrying capacity of wings of aircraft used for agricultural and military purposes within engine thrust limitations.

Irremediable

The Effect of Small Structural Changes on Optimized Active Control Systemsers are identified the designer of the control system has three options at his disposal. He can try to obtain more accurate values of the most troublesome parameters, he can redesign the control system to reduce the sensitivity or he can seek minor changes in the structure to reduce the sensitivity.

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Conference proceedings 1987Leipholz etc. , mostly in journals of ASCE, was given its fIrst international forum at the University of Waterloo, Waterloo, Ontario, Canada, via an ruTMf - Symposium held in June, 1979. This very successful event gathered experts from a variety of technical and theoretical domains in which control

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