search.noResults

search.searching

saml.title
dataCollection.invalidEmail
note.createNoteMessage

search.noResults

search.searching

orderForm.title

orderForm.productCode
orderForm.description
orderForm.quantity
orderForm.itemPrice
orderForm.price
orderForm.totalPrice
orderForm.deliveryDetails.billingAddress
orderForm.deliveryDetails.deliveryAddress
orderForm.noItems
Trans RINA, Vol 161, Part A4, Intl J Maritime Eng, Oct-Dec 2019 44.


GARG, A. K., KHARE, R. K. & KANT, T., 2006. Free vibration of skew fiber-reinforced composite and sandwich laminates using a shear deformable finite element model. Journal of Sandwich Structures & Materials, Volume 8, pp. 33-53.


45. 46.


GRUTTMANN, F. & WAGNER, W., 2017. Shear correction factors for layered plates and shells. Computational Mechanics, Volume 59, pp. 129-146.


GÜRSES, M., CIVALEK, Ö., KORKMAZ, A. K. & ERSOY, H., 2009. Free vibration analysis of symmetric laminated skew plates by discrete singular convolution technique based on first- order shear deformation theory. International journal for numerical methods in engineering, Volume 79, pp. 290-313.


47. 48.


HA, K. H., 1990. Finite element analysis of sandwich plates: an overview. Computers & Structures, Volume 37, pp. 397-403.


HE, D., YANG, W. & CHEN, W., 2017. A size- dependent composite laminated skew plate model based on a new modified couple stress theory. Acta Mechanica Solida Sinica, Volume 30, pp. 75-86.


49. 50. 51.


HENCKY, H., 1947. Uber die Berucksichtigung der Schubverzerrung in ebenen Platten. ingenieur-archiv, Volume 16, pp. 72-76.


IDLBI, A., KARAMA, M. & TOURATIER, M., 1997. Comparison of various laminated plate theories. Composite Structures, Volume 37, pp. 173-184.


JABERZADEH, E., AZHARI, M. & BOROOMAND, B., 2013. Inelastic buckling of skew and rhombic thin thickness-tapered plates with and without intermediate supports using the element-free Galerkin method. Applied Mathematical Modelling, Volume 37, pp. 6838- 6854.


52. 53. 54.


JEGLEY, D. C., 1988. An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders.


JEMIELITA, G., 1975. Technical theory of plates with moderate thickness. Rozprawy Ink, Volume 23, pp. 483-499.


JIN, G., SU, Z., SHI, S., YE, T., & GAO, S., 2014a. Three-dimensional exact solution for the free vibration of arbitrarily thick functionally graded rectangular plates with general boundary conditions. Composite Structures, Volume 108, pp. 565-577.


55.


JIN, G., SU, Z., YE, T. & JIA, X., 2014b. Three- dimensional vibration analysis of isotropic and orthotropic conical shells with elastic boundary restraints. International Journal of Mechanical Sciences, Volume 89, pp. 207-221.


56.


JIN, C. & WANG, X., 2015. Weak form quadrature element method for accurate free vibration analysis of thin skew plates. Computers


67.


& Mathematics with Applications, Volume 70, pp. 2074-2086.


57.


JIN, G., SHI, S., SU, Z., LI, S., & LIU, Z., 2015a. A modified Fourier--Ritz approach for free vibration analysis of laminated functionally graded shallow shells with general boundary conditions. International Journal of Mechanical Sciences, Volume 93, pp. 256-269.


58.


JIN, G., SU, Z., YE, T. & GAO, S., 2015b. Three-dimensional free vibration analysis of functionally graded annular sector plates with general boundary conditions. Composites Part B: Engineering, Volume 83, pp. 352-366.


59.


JIN, G., YE, T. & SHI, S., 2015c. Three- Dimensional Vibration Analysis of Isotropic and Orthotropic Open Shells and Plates with Arbitrary Boundary Conditions. Shock and Vibration, Article ID 896204.


60.


JIN, G., YE, T.,WANG, X. & MIAO, X., 2016c. A unified solution for the vibration analysis of FGM doubly-curved shells of revolution with arbitrary boundary conditions. Composites Part B 89, 230-252


61. 62. 63. 64. 65. 66.


JONES, R. M., 1975. Mechanics of composite materials. s.l.:Scripta Book Company Washington, DC.


KABIR, H. R. H., 1996. A novel approach to the solution of shear flexible rectangular plates with arbitrary laminations. Composites Part B: Engineering, Volume 27, pp. 95-104.


KALITA, K. & HALDAR, S., 2015. Parametric study on thick plate vibration using FSDT. Mechanics and Mechanical Engineering, Volume 19, pp. 81-90.


KALITA, K., SHINDE, D. & HALDAR, S., 2015. Analysis on Transverse Bending of Rectangular Plate. Materials Today: Proceedings, Volume 2, pp. 2146-2154.


KALITA, K. & HALDAR, S., 2016. Free vibration analysis of rectangular plates with central cutout. Cogent Engineering, Volume 3, p. 1163781.


KALITA, K. RAMACHANDRAN, M., RAICHURKAR, P., MOKAL, S. D., & HALDAR, S., 2016a. Free vibration analysis of laminated composites by a nine node iso- parametric plate bending element. Advanced Composites Letters, Volume 25, pp. 108-116.


KALITA, K., SHIVAKOTI, I., GHADAI, R. K. & HALDAR, S., 2016b. Rotary Inertia Effect in Isotropic Plates Part I: Uniform Thickness. Romanian Journal of Acoustics and Vibration, Volume 13, pp. 68-74.


68.


KALITA, K., SHIVAKOTI, I., GHADAI, R. K. & HALDAR, S., 2016c. Rotary Inertia Effect in Isotropic Plates Part II: Taper Thickness. Romanian Journal of Acoustics and Vibration, Volume 13, pp. 75-80.


69.


KALITA, K. & HALDAR, S., 2017. Eigenfrequencies of simply supported taper


©2019: The Royal Institution of Naval Architects


A-373


Page 1  |  Page 2  |  Page 3  |  Page 4  |  Page 5  |  Page 6  |  Page 7  |  Page 8  |  Page 9  |  Page 10  |  Page 11  |  Page 12  |  Page 13  |  Page 14  |  Page 15  |  Page 16  |  Page 17  |  Page 18  |  Page 19  |  Page 20  |  Page 21  |  Page 22  |  Page 23  |  Page 24  |  Page 25  |  Page 26  |  Page 27  |  Page 28  |  Page 29  |  Page 30  |  Page 31  |  Page 32  |  Page 33  |  Page 34  |  Page 35  |  Page 36  |  Page 37  |  Page 38  |  Page 39  |  Page 40  |  Page 41  |  Page 42  |  Page 43  |  Page 44  |  Page 45  |  Page 46  |  Page 47  |  Page 48  |  Page 49  |  Page 50  |  Page 51  |  Page 52  |  Page 53  |  Page 54  |  Page 55  |  Page 56  |  Page 57  |  Page 58  |  Page 59  |  Page 60  |  Page 61  |  Page 62  |  Page 63  |  Page 64  |  Page 65  |  Page 66  |  Page 67  |  Page 68  |  Page 69  |  Page 70  |  Page 71  |  Page 72  |  Page 73  |  Page 74  |  Page 75  |  Page 76  |  Page 77  |  Page 78  |  Page 79  |  Page 80  |  Page 81  |  Page 82  |  Page 83  |  Page 84  |  Page 85  |  Page 86  |  Page 87  |  Page 88  |  Page 89  |  Page 90  |  Page 91  |  Page 92  |  Page 93  |  Page 94  |  Page 95  |  Page 96  |  Page 97  |  Page 98  |  Page 99  |  Page 100  |  Page 101  |  Page 102  |  Page 103  |  Page 104  |  Page 105  |  Page 106  |  Page 107  |  Page 108  |  Page 109  |  Page 110  |  Page 111  |  Page 112  |  Page 113  |  Page 114  |  Page 115  |  Page 116  |  Page 117  |  Page 118  |  Page 119  |  Page 120  |  Page 121  |  Page 122  |  Page 123  |  Page 124  |  Page 125  |  Page 126  |  Page 127  |  Page 128  |  Page 129  |  Page 130  |  Page 131  |  Page 132  |  Page 133  |  Page 134  |  Page 135  |  Page 136  |  Page 137  |  Page 138  |  Page 139  |  Page 140  |  Page 141  |  Page 142  |  Page 143  |  Page 144  |  Page 145  |  Page 146  |  Page 147  |  Page 148  |  Page 149  |  Page 150  |  Page 151  |  Page 152  |  Page 153  |  Page 154  |  Page 155  |  Page 156  |  Page 157  |  Page 158  |  Page 159  |  Page 160  |  Page 161  |  Page 162  |  Page 163  |  Page 164  |  Page 165  |  Page 166