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Numerical Simulation of Blast Wave within an Open Ended Shock Tube and Its Interaction with Generic Objects for Pressure Ratios from 3 to 30

To find the blast wave profile and the mass flow generated inside the shock tube being installed in TBRL Chandigarh for pressure ratio varying from 3 to 30. Optimization of driver section length to obtain the Fried lander waveform using numerical simulation. The interaction of shock/blast wave diffracted at the open end of the shock tube with curved plates, cone and rectangular geometries.

Project Number:
GAP 161712
Project Type:
Project Date:
19/03/2015 to 18/11/2017
Cost of the Project:
16.02 Lakhs
Sponsoring Agency:
Name of Co PI: Dr. Sudipta De

Last updated : 18 Dec, 2017