Civil and military concepts are compared in relation to aircraft performance requirements and reasons for continuing need for optical transparencies are enumerated; aircraft general requirements affecting transparencies; environmental conditions; design feature considerations relating to basic glazing, interlayers, sealants, gap fillers and cushioning materials, transparency frame, and complete transparency assembly; tabulation of basic glazing materials and data on their modulus of rupture at room temperature and suggested temperature limitations for long-term use; design proposals for canopies and passenger cabin windows, windscreens, etc; test requirements and test methods.


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    Title :

    Transparencies for supersonic and hypersonic flight


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1964


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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