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


the TSDT developed by Reddy (Reddy, 1984) is the most commonly used one. The transverse shear deformation effect is considered in TSDT. It also satisfies the zero- traction boundary conditions on the top and bottom surfaces of a plate. Thus, a shear correction factor is not needed. Though the equations of motion for Reddy’s TSDT and Levinson’s theory (Levinson, 1980) are different both these theories use the same displacement field. The displacement field of Reddy’s third-order shear deformation theory may be expressed as,


= (, ) + [(, ) − 2


4 3 (


4 3 (


ℎ) ((, ) + )]


= (, ) + [(, ) − 2


ℎ) ((, ) + = (, )


)]


Where , , are displacements in , , directions respectively;


, , are unknown functions of


position(, ); and are the rotations of a transverse normal about the -axis and -axis, respectively.


Murthy (Murthy, 1981) developed a higher-order shear deformation theory and formulated it for unsymmetric laminates, symmetric laminates and classical orthotropy. In such similar attempts, a few TSDTs were formulated by Ambartsumian (Ambartsumian, 1960) (Ambartsumian, 1969), Librescu (Librescu, 1967), Shirakawa (Shirakawa, 1983) and Bhimaraddi & Stevens (Bhimaraddi & Stevens, 1984) among others. In 1984, Reddy (Reddy, 1984) reviewed all TSDTs proposed until then and established an equivalence among them. Phan & Reddy (Phan & Reddy, 1985) proposed a higher-order shear deformation theory that accounted for parabolic distribution of the transverse shear stresses. Pandya & Kant (Pandya & Kant, 1988) incorporated a linear variation of transverse normal strains and parabolic variation of transverse shear strains through plate thickness. A nine-node Lagrangian parabolic isoparametric plate bending element was used by them for the finite element analysis. Murty & Vellaichamy (Murty & Vellaichamy, 1988) developed a higher-order shear deformation theory with provision for cubic variation of in-plane displacements and parabolic variation of the normal displacement. Using the principle of virtual displacements Ren-Huai & Ling-Hui (Ren-Huai & Ling-Hui, 1991) developed a TSDT that accounted for parabolic variation of transverse shear strains through the thickness. Singh & Rao (Singh & Rao, 1996) developed a four node rectangular element with fourteen degrees of freedom and it used it in conjunction with a TSDT to study the effect of various parameters such as lay-up, side to thickness ratio, aspect ratio, type of loadings, boundary conditions on stability characteristics of laminated plates. Vuksanovic (Vuksanovic, 2000) developed a TSDT that could take a parabolic distribution of shear strains across the plate thickness and cubic variation for in-plane displacements.


A-360 (3)


Idlbi et al. (Idlbi, et al., 1997) in 1997 made a comparative study of CLPT, FSDT, TSDT and TSDPT (sine type), through which they concluded TSDPT to better than the others especially when interlayer continuity requirements are included. Much later Carrera (Carrera, 2007) compared three different TSDT models – one having five displacement variables, and the other two having three displacement variables. While the second TSDT was reduced from five displacement variables to three by enforcing homogeneous transverse stress conditions, the third was done so by considering non-homogeneous transverse stress conditions. He concluded that the use of non-homogeneous transverse stress conditions led to superiority of the third model over the second one. However, in general, the original model (first one) still had better estimations the other two.


2.3 (b) Trigonometric shear deformation theory (TgSDT)


As the name suggests, trigonometric functions are used to describe the shear deformation plate theories called trigonometric shear deformation theory (TgSDT). TgSDT is richer than polynomial functions, simple, more accurate and the stress-free surface boundary conditions can be guaranteed a priori (Mantari, et al., 2012). TgSDT was realized by Levy (Levy, 1877) using sinusoidal functions in the displacement field. The displacement field of the Levy’s TgSDT are as follows,


= ∑ 2+1


∑ (2+1) ℎ


=0


=0


= ∑ 2+1


∑ (2+1) ℎ


=0


=0


= ∑ 2


=0


(, ) + (, )


(, ) + (, )


(, )


where , , are displacements in , , directions respectively;


, , are unknown functions of


position(, ) ; and are the rotations of a transverse normal about the -axis and -axis, respectively.


Other such TgSDTs have been developed for plate and shells using sine, hyperbolic sine and cosine functions. The trigonometric functions describe the warping through the thickness of the plate during rotation due to transverse shear. Kil’chevskiy (Kil'chevskiy, 1965) in his book discussed TgSDTs in detail. He solved several static and dynamic problems on shells which were used as benchmark problems till much later. However, he neglected the dissipative forces in the analysis. Stein and Jegley (Stein & Jegley, 1987) used a TgSDT and described the displacement fields using algebraic and trigonometric terms. To find the displacements and stresses they used both potential and complementary energymethods. Jegley (Jegley, 1988) in a technical report for NASA, USA studied the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders by using a TgSDT. He also reported that the


©2019: The Royal Institution of Naval Architects (4)


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