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K R SIVADAS
- Rate J$666
- Response 1h
-
Students1
Number of students K R SIVADAS has accompanied since arriving at Superprof
Number of students K R SIVADAS has accompanied since arriving at Superprof
J$666/hr
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- Civil engineering
- Agricultural Sciences
- Electricity
- Automation
Mechanical system Design and design checking utilizing some of the Finite Element software tools, like MSC NASTRAN, LSDYNA3D, ANSYS, etc... Project management and effort estimation of design and a
- Civil engineering
- Agricultural Sciences
- Electricity
- Automation
Lesson location
About K R SIVADAS
March 1987- Feb. 1992 Dept. of Applied Mechanics, Indian Institute of Chennai, India
Technology Madras (India)
6
Institute
:
IITM is one of the well Known higher learning institutes in INDIA. IIT is involved in training and development of manpower apart from research and development in science and technology.
Dissertation topic
:
Dynamic analysis of Shells of Revolution.
(Major: Shell Vibration).
Achievements : Shells are very widely used structures in aerospace and automobiles. The analysis is concentrated for composite shells.
: The objective of this research is to investigate vibration behaviour of laminated tapered composite structures.
: This mainly involves in the understanding of vibration behavior of different types of configurations, geometric as well as material
Shells made of composite materials are analyzed for their dynamic characteristics using different shell theories. One thin and two thick shell theories are used for the solution. Various other effects like the coupling due to anisotropy of the shell material, material damping, and rotational effects also studied. A limited study on response behavior of shell due to impact load also conducted. For all these studies a semi-analytical finite element method is used as the solution procedure. The element properties and corresponding matrices are derived and coded in the computer and solved for various characteristics.
Completed the Research and the Institute awarded the diploma. I have got number of publications in international journals out of this research.
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About the lesson
- Primary
- Lower Secondary
- Upper Secondary
- +11
levels :
Primary
Lower Secondary
Upper Secondary
Lower Sixth Form
Upper Sixth Form
Diploma
Adult Education
Undergraduate
Master’s degree
PhD
Other
Legal Education Certificate (LEC)
MBA
Kindergarten
- English
All languages in which the lesson is available :
English
March 1987- Feb. 1992 Dept. of Applied Mechanics, Indian Institute of Chennai, India
Technology Madras (India)
6
Institute
:
IITM is one of the well Known higher learning institutes in INDIA. IIT is involved in training and development of manpower apart from research and development in science and technology.
Dissertation topic
:
Dynamic analysis of Shells of Revolution.
(Major: Shell Vibration).
Achievements : Shells are very widely used structures in aerospace and automobiles. The analysis is concentrated for composite shells.
: The objective of this research is to investigate vibration behaviour of laminated tapered composite structures.
: This mainly involves in the understanding of vibration behavior of different types of configurations, geometric as well as material
Shells made of composite materials are analyzed for their dynamic characteristics using different shell theories. One thin and two thick shell theories are used for the solution. Various other effects like the coupling due to anisotropy of the shell material, material damping, and rotational effects also studied. A limited study on response behavior of shell due to impact load also conducted. For all these studies a semi-analytical finite element method is used as the solution procedure. The element properties and corresponding matrices are derived and coded in the computer and solved for various characteristics.
Completed the Research and the Institute awarded the diploma. I have got number of publications in international journals out of this research.
See more
Rates
Rate
- J$666
Pack prices
- 5h: J$3330
- 10h: J$6,330
online
- J$666/h
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