Election of materials for airframe structure on SST must be established on basis of requirements which embrace efficiency in design and performance, cost-weight analysis, economical and reproducible fabrication processes, long airframe life in SST environment with extended life expectancy beyond design minimum, and minimum maintenance required during life of aircraft; static properties under short-time and long-time exposure, in relation to density of materials, are measure of structural efficiency; other properties to consider; finally, materials must be evaluated in terms of various types of structures under consideration.


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    Title :

    Structural materials for supersonic transport


    Additional title:

    J Aircraft


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English