1997
DOI: 10.1002/(sici)1097-0207(19970630)40:12<2151::aid-nme144>3.0.co;2-h
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Dynamic Animation of Stress Modes via the Integrated Force Method of Structural Analysis

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Cited by 7 publications
(7 citation statements)
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“…The animation of the stress mode shape in IFM/IFMD (ref. 22) detected a stress concentration region in the same blade due to a small hole, which is qualitatively shown in figure 8(a). Typically, stress mode shape is not available in the stiffness formulation.…”
Section: Frequency Analysis Of a Turboprop Bladementioning
confidence: 56%
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“…The animation of the stress mode shape in IFM/IFMD (ref. 22) detected a stress concentration region in the same blade due to a small hole, which is qualitatively shown in figure 8(a). Typically, stress mode shape is not available in the stiffness formulation.…”
Section: Frequency Analysis Of a Turboprop Bladementioning
confidence: 56%
“…The IFM element (ref. 22) used a total of 18 force unknowns: 4 for each normal stress and 2 for each shear stress. The brick element of a commercial code was comparable to the stiffness method of the IFM/Analyzers software.…”
Section: Frequency Analysis Of a Turboprop Bladementioning
confidence: 99%
“…The three BCC given by equation (11) CBMF is defined through the EE and the CC in the field and on the boundary of an elastic continuum, given by equations (8) to (11). Stress determination by CBMF does not require the displacement boundary conditions.…”
Section: Completed Beltrami-michell Formulationmentioning
confidence: 99%
“…11,16,17 Results for a few typical examples obtained using the IFM/Analyzers code and a commercial stiffness method code are depicted in figure 5. The three IFM elements used are (1) a four-node QUAD0405 membrane element with five force unknowns, (2) an eight-node brick element HEX0818 with 18 force unknowns, and (3) a fournode-plate bending element PLB0409 with nine unknown moments.…”
Section: Ifm/analyzers Codementioning
confidence: 99%
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