2007
DOI: 10.1017/s172771910000143x
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Optimization of Sandwich Monocoque Car Body with Equivalent Shell Element

Abstract: This research proposes a straightforward and efficient method to optimize a sandwich monocoque car body with the developed equivalent shell element based on stiffness equivalence. The fact that stiffness rather than strength is dominant constraint for ordinary car body optimization is demonstrated. A simple but heavy flat chassis plate is utilized as upper bound, while an ideal monocoque is used as lower bound for an actual car body optimization. Convergence hours can be significantly reduced with the equivale… Show more

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Cited by 3 publications
(1 citation statement)
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“…,12,18,25,28,34,38,42,47,49,59,84,122,123, 127-129,131,143,145,146,156,165,200,222,225,227,238,240,256,258,261, 265,269,272,282,283,293,315,344,351,360,403,410,412,413,419,422,423, 437,469,470,476,498,500,503,520,530,552,563,565,568,583,592,595,607, 615,620,632,640,641,674,665,724,726,741,745,761,765,771,793,802,812, 848,858,860,861,876,884,911,913,915,923,944,965,970,977,992,1004 twist angle, 217,741,913 curvatures, 324,588 laminate strain components, " xx , " yy , or xx , 192,226,404,491,495,637,717,727, 761,836,859,897,912,922,981 strain energy,820,876,953 or a lower limit on extensional stiffness terms, A ij ,17,35,113,198,317,543,554,589 transverse shear stiffness,113,925 torsional and/or bending stiffness,62,71,81,93,96,105,106,176,178, 230,274,292,554,747,825 axial stiffness,566,947 prebuckling and/or postbuckling stiffness,686 elastic moduli,86,95,110, 117,162,291,377,378,386,408,424,431,514,545,747,1002 stiffness coefficients, 427 bulk modulus,…”
mentioning
confidence: 99%
“…,12,18,25,28,34,38,42,47,49,59,84,122,123, 127-129,131,143,145,146,156,165,200,222,225,227,238,240,256,258,261, 265,269,272,282,283,293,315,344,351,360,403,410,412,413,419,422,423, 437,469,470,476,498,500,503,520,530,552,563,565,568,583,592,595,607, 615,620,632,640,641,674,665,724,726,741,745,761,765,771,793,802,812, 848,858,860,861,876,884,911,913,915,923,944,965,970,977,992,1004 twist angle, 217,741,913 curvatures, 324,588 laminate strain components, " xx , " yy , or xx , 192,226,404,491,495,637,717,727, 761,836,859,897,912,922,981 strain energy,820,876,953 or a lower limit on extensional stiffness terms, A ij ,17,35,113,198,317,543,554,589 transverse shear stiffness,113,925 torsional and/or bending stiffness,62,71,81,93,96,105,106,176,178, 230,274,292,554,747,825 axial stiffness,566,947 prebuckling and/or postbuckling stiffness,686 elastic moduli,86,95,110, 117,162,291,377,378,386,408,424,431,514,545,747,1002 stiffness coefficients, 427 bulk modulus,…”
mentioning
confidence: 99%