Modeling and Design for a Intelligent Three-Level Boost Converter
p.11
p.11
Flow Field Study of Sodium Aluminate Solution Slurry in an Unagitated Precipitation Tank by CFD Simulation
p.16
p.16
Affection of High Sulfur and Naphthenic Acid Crude Oil Acted on Refinery Equipment
p.21
p.21
Numerical Analysis of High Power Marine Diesel Engine Main Bearing Load and Lubricating Properties
p.25
p.25
Investigation on Residual Strength of Airplane Plate with Smooth Circular Hole
p.31
p.31
Research on Acoustic Emission Signal Processing of Concrete Beam in Fracture Experiment Based on the HHT
p.35
p.35
The Application of ROV for the Subsea Christmas Tree Installation in the LiWan3-1 Deepwater Oilfield
p.39
p.39
Numerical Simulation of Flotation Circuit for Kakoxene Ore Processing
p.43
p.43
GLC Coating Improving the Wear Resistance of Aeroengine Bearings in Insufficient Lubrication
p.48
p.48
Investigation on Residual Strength of Airplane Plate with Smooth Circular Hole
Abstract:
In order to solve the fight problem of damaged airplane in war, based on linear elasticity, elastoplasticity and net section yield criterion, the calculation model for residual strength of plate with smooth circular hole is founded. Furthermore, the flexibility of calculation models using these three methods is analyzed through examples. All above can be basis for airplane battle damage assessment.
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Periodical:
Applied Mechanics and Materials (Volume 331)
Pages:
31-34
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Online since:
July 2013
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© 2013 Trans Tech Publications Ltd. All Rights Reserved
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