Nonlinear analysis of rectangular laminated plates: Dynamic relaxation analysis of small and large deflection rectangular laminates

 
9783659767876: Nonlinear analysis of rectangular laminated plates: Dynamic relaxation analysis of small and large deflection rectangular laminates
View all copies of this ISBN edition:
 
 

Dynamic Relaxation method coupled with finite differences is used for the analysis of rectangular laminates. In this method, the equilibrium equations are converted to dynamic equations by adding damping and inertia terms. These are then expressed in finite differences form and the solution is obtained by an iterative procedure.The functions of the DR program are as follows: read the data file, compute the stiffness of the laminate, the fictitious densities, the velocities and displacements and the mid-plane deflections and stresses, check the stability of the numerical computations, convergence of the solution, and the wrong convergence, compute through thickness stresses in direction of plate axes, and transform through thickness stresses in the lamina principal axes. The errors inherent in the DR technique include discretization error which is due to the replacement of a continuous function with a discrete function, and an additional error due to the non-exact solution of the discrete equations. The present DR results are compared with similar studies to validate the DR program, and the results are found of acceptable accuracy.

"synopsis" may belong to another edition of this title.

About the Author:

Osama Mohammed was born in Atbara in 1966.He received his bachelor degree in mechanical engineering from Sudan university of science and technology,Faculty of engineering in 1998, and a master degree in solid mechanics from Nile valley university in 2003.He contributed in teaching some subjects in other universities in different parts of Sudan.

"About this title" may belong to another edition of this title.

Buy New View Book
List Price: US$ 65.00
US$ 51.03

Convert currency

Shipping: US$ 5.00
From United Kingdom to U.S.A.

Destination, rates & speeds

Add to Basket

Top Search Results from the AbeBooks Marketplace

1.

Osama Mohammed Elmardi
Published by LAP Lambert Academic Publishing (2016)
ISBN 10: 3659767875 ISBN 13: 9783659767876
New Paperback Quantity Available: 1
Print on Demand
Seller:
Ria Christie Collections
(Uxbridge, United Kingdom)
Rating
[?]

Book Description LAP Lambert Academic Publishing, 2016. Paperback. Condition: New. PRINT ON DEMAND Book; New; Publication Year 2016; Not Signed; Fast Shipping from the UK. No. book. Seller Inventory # ria9783659767876_lsuk

More information about this seller | Contact this seller

Buy New
US$ 51.03
Convert currency

Add to Basket

Shipping: US$ 5.00
From United Kingdom to U.S.A.
Destination, rates & speeds

2.

Osama, Mohammed Elmardi
Published by LAP Lambert Academic Publishing (2015)
ISBN 10: 3659767875 ISBN 13: 9783659767876
New Quantity Available: > 20
Print on Demand
Seller:
Pbshop
(Wood Dale, IL, U.S.A.)
Rating
[?]

Book Description LAP Lambert Academic Publishing, 2015. PAP. Condition: New. New Book. Shipped from US within 10 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Seller Inventory # IQ-9783659767876

More information about this seller | Contact this seller

Buy New
US$ 58.74
Convert currency

Add to Basket

Shipping: US$ 3.99
Within U.S.A.
Destination, rates & speeds

3.

Osama, Mohammed Elmardi
ISBN 10: 3659767875 ISBN 13: 9783659767876
New Quantity Available: 1
Seller:
Rating
[?]

Book Description Condition: New. Publisher/Verlag: LAP Lambert Academic Publishing | Dynamic relaxation analysis of small and large deflection rectangular laminates | Dynamic Relaxation method coupled with finite differences is used for the analysis of rectangular laminates. In this method, the equilibrium equations are converted to dynamic equations by adding damping and inertia terms. These are then expressed in finite differences form and the solution is obtained by an iterative procedure.The functions of the DR program are as follows: read the data file, compute the stiffness of the laminate, the fictitious densities, the velocities and displacements and the mid-plane deflections and stresses, check the stability of the numerical computations, convergence of the solution, and the wrong convergence, compute through thickness stresses in direction of plate axes, and transform through thickness stresses in the lamina principal axes. The errors inherent in the DR technique include discretization error which is due to the replacement of a continuous function with a discrete function, and an additional error due to the non-exact solution of the discrete equations. The present DR results are compared with similar studies to validate the DR program, and the results are found of acceptable accuracy. | Format: Paperback | Language/Sprache: english | 128 pp. Seller Inventory # K9783659767876

More information about this seller | Contact this seller

Buy New
US$ 59.72
Convert currency

Add to Basket

Shipping: US$ 3.43
From Germany to U.S.A.
Destination, rates & speeds

4.

Osama Mohammed Elmardi
Published by LAP Lambert Academic Publishing (2015)
ISBN 10: 3659767875 ISBN 13: 9783659767876
New Quantity Available: > 20
Print on Demand
Seller:
Books2Anywhere
(Fairford, GLOS, United Kingdom)
Rating
[?]

Book Description LAP Lambert Academic Publishing, 2015. PAP. Condition: New. New Book. Delivered from our UK warehouse in 3 to 5 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Seller Inventory # LQ-9783659767876

More information about this seller | Contact this seller

Buy New
US$ 55.13
Convert currency

Add to Basket

Shipping: US$ 11.67
From United Kingdom to U.S.A.
Destination, rates & speeds

5.

Osama Mohammed Elmardi
Published by LAP Lambert Academic Publishing, United States (2015)
ISBN 10: 3659767875 ISBN 13: 9783659767876
New Paperback Quantity Available: 10
Print on Demand
Seller:
The Book Depository EURO
(London, United Kingdom)
Rating
[?]

Book Description LAP Lambert Academic Publishing, United States, 2015. Paperback. Condition: New. Language: English . Brand New Book ***** Print on Demand *****.Dynamic Relaxation method coupled with finite differences is used for the analysis of rectangular laminates. In this method, the equilibrium equations are converted to dynamic equations by adding damping and inertia terms. These are then expressed in finite differences form and the solution is obtained by an iterative procedure.The functions of the DR program are as follows: read the data file, compute the stiffness of the laminate, the fictitious densities, the velocities and displacements and the mid-plane deflections and stresses, check the stability of the numerical computations, convergence of the solution, and the wrong convergence, compute through thickness stresses in direction of plate axes, and transform through thickness stresses in the lamina principal axes. The errors inherent in the DR technique include discretization error which is due to the replacement of a continuous function with a discrete function, and an additional error due to the non-exact solution of the discrete equations. The present DR results are compared with similar studies to validate the DR program, and the results are found of acceptable accuracy. Seller Inventory # AAV9783659767876

More information about this seller | Contact this seller

Buy New
US$ 77.43
Convert currency

Add to Basket

Shipping: US$ 3.89
From United Kingdom to U.S.A.
Destination, rates & speeds

6.

Mohammed Elmardi Osama
Published by LAP Lambert Academic Publishing Sep 2015 (2015)
ISBN 10: 3659767875 ISBN 13: 9783659767876
New Taschenbuch Quantity Available: 1
Seller:
BuchWeltWeit Inh. Ludwig Meier e.K.
(Bergisch Gladbach, Germany)
Rating
[?]

Book Description LAP Lambert Academic Publishing Sep 2015, 2015. Taschenbuch. Condition: Neu. Neuware - Dynamic Relaxation method coupled with finite differences is used for the analysis of rectangular laminates. In this method, the equilibrium equations are converted to dynamic equations by adding damping and inertia terms. These are then expressed in finite differences form and the solution is obtained by an iterative procedure.The functions of the DR program are as follows: read the data file, compute the stiffness of the laminate, the fictitious densities, the velocities and displacements and the mid-plane deflections and stresses, check the stability of the numerical computations, convergence of the solution, and the wrong convergence, compute through thickness stresses in direction of plate axes, and transform through thickness stresses in the lamina principal axes. The errors inherent in the DR technique include discretization error which is due to the replacement of a continuous function with a discrete function, and an additional error due to the non-exact solution of the discrete equations. The present DR results are compared with similar studies to validate the DR program, and the results are found of acceptable accuracy. 128 pp. Englisch. Seller Inventory # 9783659767876

More information about this seller | Contact this seller

Buy New
US$ 64.83
Convert currency

Add to Basket

Shipping: US$ 19.64
From Germany to U.S.A.
Destination, rates & speeds

7.

Mohammed Elmardi Osama
Published by LAP Lambert Academic Publishing Sep 2015 (2015)
ISBN 10: 3659767875 ISBN 13: 9783659767876
New Taschenbuch Quantity Available: 1
Seller:
Rheinberg-Buch
(Bergisch Gladbach, Germany)
Rating
[?]

Book Description LAP Lambert Academic Publishing Sep 2015, 2015. Taschenbuch. Condition: Neu. Neuware - Dynamic Relaxation method coupled with finite differences is used for the analysis of rectangular laminates. In this method, the equilibrium equations are converted to dynamic equations by adding damping and inertia terms. These are then expressed in finite differences form and the solution is obtained by an iterative procedure.The functions of the DR program are as follows: read the data file, compute the stiffness of the laminate, the fictitious densities, the velocities and displacements and the mid-plane deflections and stresses, check the stability of the numerical computations, convergence of the solution, and the wrong convergence, compute through thickness stresses in direction of plate axes, and transform through thickness stresses in the lamina principal axes. The errors inherent in the DR technique include discretization error which is due to the replacement of a continuous function with a discrete function, and an additional error due to the non-exact solution of the discrete equations. The present DR results are compared with similar studies to validate the DR program, and the results are found of acceptable accuracy. 128 pp. Englisch. Seller Inventory # 9783659767876

More information about this seller | Contact this seller

Buy New
US$ 64.83
Convert currency

Add to Basket

Shipping: US$ 19.64
From Germany to U.S.A.
Destination, rates & speeds