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  • Structural Mechanics  (2)
  • 1985-1989
  • 1945-1949  (2)
  • 1946  (2)
  • 1
    Publication Date: 2019-06-28
    Description: The theory of Lagrangian multipliers is applied to the problem of finding both upper and lower limits to the true compressive buckling stress of a clamped rectangular plate. The upper and lower limits thus bracket the truss, which cannot be exactly found by the differential-equation approach. The procedure for obtaining the upper limit, which is believed to be new, presents certain advantages over the classical Raleigh-Rite method of finding upper limits. The theory of the lower-limit procedure has been given by Trefftz but, in the present application, the method differs from that of Trefftz in a way that makes it inherently more quickly convergent. It is expected that in other buckling problems and in some vibration problems problems the Lagrangian multiplier method finding upper and lower limits may be advantageously applied to the calculation of buckling stresses and natural frequencies.
    Keywords: Structural Mechanics
    Type: AD-A301132 , NACA-TR-848 , NASA-TM-111368 , NAS 1.15:111368
    Format: application/pdf
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  • 2
    Publication Date: 2019-08-17
    Description: The present paper deals with the computation and methods of reinforcement of stiffened panels with cutouts under bending loads such as are applied to the sides of a fuselage. A comparison is maade between the computed and test results. Results are presented of tests on panels with cutouts under tensile and compressive loads.
    Keywords: Structural Mechanics
    Type: NACA-TM-1094 , ; 454
    Format: application/pdf
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