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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    Title :

    Bending and compression tests of pressurized ring-stiffened cylinders


    Additional title:

    NASA -- Tech Note


    Contributors:
    Dow, M.B. (author) / Peterson, J.P. (author)


    Publication date :

    1960


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    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