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Article title NUMERICAL METHOD OF PREDICTING THE COMPLEX STRESS-STRAINED STATE OF THE FLIGHT VEHICLES CONSTRUCTIONS
Authors O.G. Osiaev, R.A. Neydorf
Section SECTION V. PILOTLESS FLYING DEVICES
Month, Year 03, 2010 @en
Index UDC 593.3
DOI
Abstract The systems of equations of the prognostication of the complex stress-strained state of multi-layer constructions are obtained and are examined the methods of their solutions, which can be used for the physically nonlinear tasks of thermoelasticity and heat resilience for the multifactor static and dynamic load of the shells of flight vehicles from the polymeric composites under operating conditions.

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Keywords Numerical method; prognostication; shell; the stress-strained state; flight vehicle.
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