Automated modelling, simulation of crack growth and estimation of residual strength of stiffened fuselage panels with multisite damage by K. V. N. Gopal

By: Material type: BookBookSeries: IISc, Dept of AE, PhD ThesisPublication details: Bangalore Indian Institute of Science 2001Description: ix,195pSubject(s): DDC classification:
  • 629.13434 P01 "THESIS"
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Item type Current library Call number Status Date due Barcode
Thesis Thesis JRD Tata Memorial Library 629.13434 P01 "THESIS" (Browse shelf(Opens below)) Available T05112

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