This report presents the results of a study to design and fabricate a radiative actively cooled panel. The panel assembly consists of an external thermal protection system (metallic heat shields and insulation blankets) and an aluminum honeycomb structure.
Design and Fabrication of a Radiative Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft
1978
157 pages
Report
Keine Angabe
Englisch
Aircraft , Nonferrous Metals & Alloys , Heat shields , Hypersonic aircraft , Aircraft panels , Liquid cooling , Optimization , Aluminum alloys , Structural analysis , Fabrication , Radiative transfer , Crack propagation , Shear stresses , Cooling and ventilating equipment , Coolants , Design criteria , Heat flux , Aerothermodynamics , Surface temperature , Skin(Structural) , Aerodynamic heating , Thermal cycling tests , Dynamic pressure , Thermal stresses , Heat sinks , Fatigue tests(Mechanics) , Axial loads , Cyclic loads , Sandwich panels , Honeycomb structures , Ethylene glycol , Thermal insulation , Heat resistant alloys , Structural integrity , Active cooling