Astronomy & Space Sciences
Title : | Deformation and Failure of Containment System Materials for High Speed Rotating Aircraft Systems |
Area of research : | Astronomy & Space Sciences |
Principal Investigator : | Prof. Krishna N. Jonnalagadda, Indian Institute Of Technology Bombay, Maharashtra |
Timeline Start Year : | 2023 |
Timeline End Year : | 2025 |
Contact info : | krishnajn@iitb.ac.in |
Details
Executive Summary : | In this project, a series of experiments on aircraft containment system material, with yield strength greater than 1000 MPa, will be conducted to extract constitutive and failure model parameters. The model will then be implemented in a numerical simulation for validation of tensile failure, and projectile impact at the coupon and component level. The primary challenges involve multiaxial and high strain rate experiments, with in situ diagnostics involving high-speed optical and thermal imaging, which are important in order to validate the model being used to capture the elasto-plastic behavior of the material. The specific model used for aircraft containment system will then be extended to armour steels used in armoured personel vehicles in India. |
Co-PI: | "Dr. Salil Shreekant Kulkarni
Indian Institute Of Technology Bombay, Maharashtra,Iit Po Powai,Maharashtra,Mumbai-400076" |
Total Budget (INR): | 49,95,600 |
Organizations involved
Implementing Agency : | Indian Institute Of Technology Bombay, Maharashtra
|
Funding Agency : | ANRF/SERB
|
Related Research