This paper is published in Volume-3, Issue-3, 2017
Area
Data Mining
Author
Anurag Manni, Naman Jaiswal, Nayan Jaiswal
Org/Univ
Shri Ramdeobaba College of Engineering and Management, Nagpur, India
Keywords
Sentiment Analysis, Rating, Review, Language Processing, E-Commerce.
Citations
IEEE
Anurag Manni, Naman Jaiswal, Nayan Jaiswal. Product Rating Based On Review, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.
APA
Anurag Manni, Naman Jaiswal, Nayan Jaiswal (2017). Product Rating Based On Review. International Journal of Advance Research, Ideas and Innovations in Technology, 3(3) www.IJARIIT.com.
MLA
Anurag Manni, Naman Jaiswal, Nayan Jaiswal. "Product Rating Based On Review." International Journal of Advance Research, Ideas and Innovations in Technology 3.3 (2017). www.IJARIIT.com.
Anurag Manni, Naman Jaiswal, Nayan Jaiswal. Product Rating Based On Review, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.
APA
Anurag Manni, Naman Jaiswal, Nayan Jaiswal (2017). Product Rating Based On Review. International Journal of Advance Research, Ideas and Innovations in Technology, 3(3) www.IJARIIT.com.
MLA
Anurag Manni, Naman Jaiswal, Nayan Jaiswal. "Product Rating Based On Review." International Journal of Advance Research, Ideas and Innovations in Technology 3.3 (2017). www.IJARIIT.com.
Abstract
This paper borders around the analysis of turbine blade static structural and modal vibration analysis. The blade is a rotating part which converts kinetic energy into mechanical energy. The turbine blade is a critical part of the turbocharger which has shown increasing development of failure destructive turbine disk. It deals with Static and vibration analysis of turbine blade which is made up of Titanium alloy to estimate its performance. The causes of failure for turbine blade have also been found out. The investigation has been done using CATIA and ANSYS 14.5 software. CATIA is used for modeling of turbine blade and analysis has been done by ANSYS 14.5 software. An effort has been made to investigate the effect of induced stresses, pressure and mode shapes at the various natural frequency on the turbine blade. A static structural analysis has been carried out to investigate the stresses and displacements of the turbine blade. A modal analysis has been carried out to investigate the mode shape and natural frequency for the designed tapered gas turbine blade.
