Computational design of actively-cooled microvascular composite skin panels for hypersonic aircraft

Keyphrases

• Design Parameters 100%
• Coolant 100%
• Microvascular Composites 100%
• Actively-cooled 100%
• Computational Design 100%
• Composite Skins 100%
• Hypersonic Aircraft 100%
• Skin Panel 100%
• Finite Element Method 50%
• Composite Panel 50%
• Thermal Response 50%
• Temperature Field 50%
• Straight Microchannel 50%
• Stabilization Schemes 50%
• 3D Weaving 50%
• Pressure Drop 50%
• Coolant Types 50%
• Thermal Load 50%
• Spurious Oscillations 50%
• Mesh Independent 50%
• Void Volume Fraction 50%
• Embedded Microchannel 50%
• Aircraft Application 50%
• Streamline Upwind Petrov-Galerkin 50%
• Numerical Solver 50%
• Design Charts 50%
• Maximum Allowable Temperature 50%
• Cooling Efficiency 50%
• Convective Heat Transfer 50%
• Microvascular System 50%

Engineering

• Microchannel 100%
• Hypersonic Vehicles 100%
• Skin Panel 100%
• Design Parameter 33%
• Finite Element Method 16%
• Composite Panel 16%
• Convective 16%
• Streamlines 16%
• Pressure Drop 16%
• Temperature Field 16%
• Thermal Load 16%
• Optimal Value 16%
• Optimal Set 16%
• Aerospace Engineering 16%