Accession Number : ADA319758

Title :   Computational Damage Model for Layered Composite Materials: Numerical Modeling of Dynamical Deforming of Damageable Thermoviscoelastic Composite Shell in Internal Loading.

Descriptive Note : Final rept.,

Corporate Author : EUROPEAN OFFICE OF AEROSPACE RESEARCH AND DEVELOPMENT FPO NEW YORK 09510

Personal Author(s) : Smirnov, N. N. ; Kiselev, A. B. ; Dimitrienko, I. D. ; Dushin, V. R.

PDF Url : ADA319758

Report Date : 03 DEC 1996

Pagination or Media Count : 168

Abstract : This report results from a contract tasking Moscow State University as follows: The contractor will create a new mathematical model for dynamical deforming and failure of viscoelastic damageable unidirectional laminated composites as detailed in his proposal dated 28 Dec 95.

Descriptors :   *LAMINATES, *DEFORMATION, MATHEMATICAL MODELS, LOAD DISTRIBUTION, STRESS ANALYSIS, SHOCK WAVES, VISCOELASTICITY, DAMAGE ASSESSMENT, GAS DYNAMICS, FRACTURE(MECHANICS), SHEAR STRESSES, HYDRODYNAMIC CODES, RUSSIA, FAILURE(MECHANICS), PRESSURE DISTRIBUTION, THERMAL STRESSES, DELAMINATION, INTERNAL PRESSURE, THERMOELASTICITY.

Subject Categories : Laminates and Composite Materials
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE