Automated modelling, simulation of crack growth and estimation of residual strength of stiffened fuselage panels with multisite damage by K. V. N. Gopal
Material type:![Book](/opac-tmpl/lib/famfamfam/BK.png)
- 629.13434 P01 "THESIS"
Item type | Current library | Call number | Status | Date due | Barcode |
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JRD Tata Memorial Library | 629.13434 P01 "THESIS" (Browse shelf(Opens below)) | Available | T05112 |
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