The Material Ablation Conduction Erosion (MACE)© program solves the 1-D heat conduction equation, including mechanisms that control internal decomposition. The surface boundary can be determined by simple conduction, constant temperature sublimation, a Munson-Spindler-type relationship, a C-3 carbon-oxygen reaction, or a generalized chemistry boundary condition. In addition to the above boundary conditions, the surface material can be removed by mechanical erosion.
Convective heat transfers and boundary layer properties can be input directly or input through a files link with an aeroheating program. Heating rates can be modified by angle-of-attack, surface roughness, non-isothermal wall, or protuberance heating.
Stuart Dunn
Senior Research Engineer
Software & Engineering Associates, Inc.
333 S. Carson Meadows Dr.
Suite 44
Carson City, NV 89701
USA
702-882-1966
702-882-1827 (fax)
stu@seainc.com
For applications in related solution areas, see the following indices: Aerospace, Heat/Fluid/Electro-magnetic Flow, Mechanical/Fluids CAE, Rocket Propulsion, SRM - Solid Rocket Motor, Spacecraft Design Tools, Thermomechanical Analysis, the developer index for Software & Engineering Associates, Inc. and the market segment index for Computational Fluid Dynamics (CFD).
Material Ablation Conduction Erosion (MACE) is a Copyright of Software & Engineering Associates
