Results obtained at high values of internal pressure differ from those obtained previously in that theoretical small-deflection compressive buckling coefficient of 0.6 was nearly achieved in each test; small amounts of internal pressure had greater stabilizing effect in bending than in compression tests; pertinence to fuselage for aircraft or missiles if expected air- and maneuver-loads are small.


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    Titel :

    Bending and compression tests of pressurized ring-stiffened cylinders


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Dow, M.B. (Autor:in) / Peterson, J.P. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Bending and compression tests of pressurized ring-stiffened cylinders

    Dow, Marvin B. / Peterson, James P. | TIBKAT | 1960


    Bending tests of ring-stiffened circular cylinders

    Peterson, James P. | TIBKAT | 1956


    Bending tests of large-diameter ring-stiffened corrugated cylinders

    Peterson, James P. / Anderson, James Kent | TIBKAT | 1966


    Bending Tests of Large-Diameter Ring-Stiffened Corrugated Cylinders

    J. K. Anderson / J. P. Peterson | NTIS | 1966