Techzilon
Aircraft-Fuselage-Analysis
Bulkhead-of-an-aircraft_CAE

Aircraft Fuselage Analysis

Strength Analysis and Optimization of the Bulkhead of an Aircraft

SKU: CAEPROJ02 Category:

Product Description

Bulkhead is the cross-wall located at various sections of the fuselage of an aircraft. Bulkheads contribute to the structural stability and rigidity of the aircraft. It also forms the main structure of the fuselage that accommodates the passenger and cargo. The bulkhead is continuously subjected to various loads during flight as well as after landing. The integrity of the bulkhead and hence airframe is very important for the safety of the aircraft.

This project aims to design and optimize the bulkhead for static and dynamic loads for optimal stiffness with maximum strength to weight ratio. For this purpose, CAE simulations will be performed on a the bulkhead model using static and dynamic conditions and based on the response of the model, topology optimization would be performed using HYPERMESH and RADIOSS software.

Based on the optimization runs, the best-fit design of the bulkhead will be identified.

About Techzilon

TECHZILON, with its strong experience offers rich-guidance and can help you achieve your career goals. TECHZILON has articulately designed the courseware by keeping in mind the requirements and expectations of the industry. The training would not only increase the theoretical understanding of the students, but will also enrich them by imparting applied and practical knowledge which is used in real industries. This will be achieved through hands on learning, training on live scenario projects and interaction with practicing industry experts.Our expert team can help you get onboard a job with leading MNCs in India and Abroad.

TECHZILON : Authorised Training Partners for HYPERMESH & ANSYS WORKBENCH

december, 2018

No Events

top
X