37 research outputs found

    Compatibility Aspects of Active Control Technologies with Aircraft Structure Design

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    Reduction of the ultimate factor by applying a maximum load concept

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    Integrated design of structures

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    Reduction of the ultimate factor by applying a maximum load concept

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    SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische InformationsbibliothekDEGerman

    Structural Aspects of Active Control Technology.

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    A survey on the structural relevant applications of Active Control Technology is presented. The benefits and disadvantages of various active control systems for transport and fighter aircraft are discussed. The problem of adverse structural coupling is addressed and possible solutions are outlined. The Smart Structure Technology offers new applications for active control technology, but to exploit the full potential of this technology multidisciplinary design methods have to be improved

    Ultimate factor for structural design of modern fighters

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    SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische InformationsbibliothekDEGerman

    Thirty years of structural dynamic investigations at MBB-UF

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    SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische InformationsbibliothekDEGerman

    Mathematical optimization - a powerful tool for aircraft design

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    With 43 figs., 24 refs.SIGLEAvailable from TIB Hannover: RO 4814(478) / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische InformationsbibliothekDEGerman
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