Microvascular composite skin panels for hypersonic aircraft

Keyphrases

• Microvascular Composites 100%
• Actively-cooled 100%
• Interface-enriched Generalized Finite Element Method 100%
• Composite Skins 100%
• Hypersonic Aircraft 100%
• Skin Panel 100%
• Composite Panel 50%
• Multiphysics 50%
• Stiffness 50%
• Mid-plane 50%
• Mechanical Properties 50%
• Numerical Examples 50%
• Channel Architecture 50%
• Thermal Response 50%
• Active Cooling 50%
• Performance Properties 50%
• Finite Element Discretization 50%
• Two-channel 50%
• 3D Weaving 50%
• Computational Design 50%
• Numerical Scheme 50%
• Embedded Microchannel 50%
• Aircraft Application 50%
• Eight-channel 50%
• Non-matching Meshes 50%
• Assessment Design 50%
• Design Sensitivity 50%
• Adaptive Extension 50%
• Computational Design Tools 50%
• Cooling Performance 50%
• Microchannel Geometry 50%
• Thermal Solver 50%
• Four-point Bending Test 50%
• Gradient-based 50%

Engineering

• Microchannel 100%
• Finite Element Method 100%
• Hypersonic Vehicles 100%
• Skin Panel 100%
• Composite Panel 33%
• Numerical Example 33%
• Active Cooling 33%
• Simplifies 33%
• Element Discretisation 33%
• Bottom Surface 33%
• Channel Geometry 33%
• Numerical Scheme 33%
• Aerospace Engineering 33%
• Design Tool 33%
• Cooling Performance 33%
• Point Bending Test 33%