The changes in the political and strategic situation in the world, especially in Europe, result in new kinds of military scenarios and in different approaches to well-known scenarios. In combination with technological advances and with new mathematical and physical solutions for system component design and for improvements in system performance this leads to a request for advanced and new types of missiles with corresponding design goals and criteria. From such more general demands associated with the overall system design new requirements for the aerodynamical and aeromechanical design goals can be derived in correspondence. Advanced experimental and theoretical tools support the project aerodynamicist in coping with these new problems. Examples for the demands for new missile types and for the new system requirements are given. The most important aeromechanical work packages in the design procedure of modern missiles are identified and methods to get solutions sufficient for qualitative answers in early project phases are presented.


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    Title :

    Aeromechanical Design of Modern Missiles


    Contributors:
    P. Hennig (author) / P. G. Lacau (author)

    Publication date :

    1994


    Size :

    76 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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