This paper is published in Volume-6, Issue-3, 2020
Area
Aerospace
Author
Raj Pranav
Co-authors
Ashok Kanna, Akshay Kumar, Ajith Raj R.
Org/Univ
Malla Reddy College of Engineering and Technology, Secunderabad, Telangana, India
Pub. Date
11 May, 2020
Paper ID
V6I3-1168
Publisher
Keywords
Thin cylindrical shells, Cutouts, Buckling behavior, Aerospace applications

Citationsacebook

IEEE
Raj Pranav, Ashok Kanna, Akshay Kumar, Ajith Raj R.. Evaluation of bucking characteristics of thin cylindrical shells with cutouts for aerospace applications, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.

APA
Raj Pranav, Ashok Kanna, Akshay Kumar, Ajith Raj R. (2020). Evaluation of bucking characteristics of thin cylindrical shells with cutouts for aerospace applications. International Journal of Advance Research, Ideas and Innovations in Technology, 6(3) www.IJARIIT.com.

MLA
Raj Pranav, Ashok Kanna, Akshay Kumar, Ajith Raj R.. "Evaluation of bucking characteristics of thin cylindrical shells with cutouts for aerospace applications." International Journal of Advance Research, Ideas and Innovations in Technology 6.3 (2020). www.IJARIIT.com.

Abstract

The aerospace industry finds a wide application of thin cylindrical shells. Cutouts in various structures are also an important application particularly in aircraft and aerospace industry which is a significant area of research today. The load-carrying capacity of these structures is determined by the buckling characteristics of that specimen mainly in aircraft since the primary cause of failure is elastic buckling. Even though cut-outs in these structures decrease the buckling strength due to the stress concentrations, it cannot be avoided in many engineering applications particularly in aircraft components. Cylindrical shells made of mild steel are considered for the study. In this paper the buckling behavior of the shells made without cutouts, with cutouts, and with semi cutouts of constant diameter are studied.
Paper PDF