A layer-wise formulation for transient response of composite sandwich panel in the exposure of thermal shock loading by considering novel linear and torsional elastic foundation

Engineering

• Transient Analysis 100%
• Shock Loads 100%
• Directional 50%
• Carbon Nanotube 50%
• Laplace Transform 50%
• Time History 50%
• Parametric Study 50%
• Dimensional Form 50%
• Radial Direction 50%
• Transients 50%
• Elasticity Theory 50%
• Sandwich Structures 50%
• Structural Design 50%

Material Science

• Composite Material 100%
• Thermal Shock 100%
• Shock Loads 100%
• Carbon Nanotube 33%
• Thermoelastic Behavior 33%