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Model updating & aeroelastic control of delaminated aircraft structures

Implementing Organization

Indian Institute of Technology (IIT), Dhanbad, Jharkhand
Principal Investigator
Dr. Prashanta kr Mahato
Indian Institute of Technology (IIT), Dhanbad, Jharkhand
CO-Principal Investigator
Dr. MUNIRATHINAM NETHAJI Indian Institute Of Science
Karnataka, Bengaluru Urban-560012
Bangalore, Karnataka, Cv Raman Road

About

An advanced aeroelastic model (plate/box beam) of delaminated aircraft structure will be developed using unified theory. The flutter analysis and control of the structure will also be performed under hygrothermal environment. The Gust response analysis of delaminated structure will also be performed. AFC will be used as sensor and actuator to control the aeroelastic response of damage structure. The studies also includes optimal placement of sensor and actuator and use of various control analysis.Finally, a modal analysis of delaminated plate will be performed to model upgraded of aeroelastic structure.

Patents

11

Publications

3

Source

Source
As received from SERB

Related Research

View All
Funding Organization
Funding Organization
Science and Engineering Research Board (SERB), New Delhi
Anusandhan National Research Foundation (ANRF)
Quick Information
Area of Research
Engineering Sciences
Focus Area
Structural health monitoring, aeroelasticity
Start Year
2019
End Year
2022
Sanction Amount
₹ 46.80 L
Status
Completed
Contact
pkmahato@gmail.com
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
00
No. of Patents
Filed : 00
Grant : 00
Disclaimer: Information available on this portal is sourced from various organizations and is provided for informational purposes only. Users are advised to verify details from the respective official sources.
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