Methods of analyzing and predicting structural weight of aircraft and missiles; methods by which minimum weight can be determined for any material and conditions of loading; principles of design for minimum weight utilized to derive weight equations for wing and fuselage structures; reports prepared in investigation of new materials and extreme operating conditions included. Eng Soc Lib. ($8.50)


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    Titel :

    Weight-strength analysis of aircraft structures


    Weitere Titelangaben:

    Weight-Strength Analysis of Aircraft Structures



    Erscheinungsdatum :

    1952


    Format / Umfang :

    394 pages


    Medientyp :

    Buch


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Weight-strength analysis of aircraft structures

    Shanley, Francis R. | SLUB | 1952




    Practical Design of Minimum-Weight Aircraft Structures for Strength and Flutter Requirements

    Keith Wilkinson / Edwin Lerner / Ronald F. Taylor | AIAA | 1976


    Eliminating unnecessary weight in aircraft structures

    Boe, M. | Engineering Index Backfile | 1942