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Configuration-Based Aerodynamics (CBAero)
A NASA software catalog entry available for reuse or request.
About this technology
Overview
CBAero is a software tool for the prediction of the conceptual aero-thermodynamic environments of aerospace configurations. The vehicle geometry is defined using unstructured, triangulated surface meshes. For subsonic Mach numbers a fast, unstructured, multi-pole panel code is coupled with a streamline tracing formulation to define the viscous surface solution. For supersonic and hypersonic Mach numbers, various independent panel methods are coupled with the streamline tracing formulation, attachment line detection methods, and stagnation-attachment line heating models to define the viscous aero-thermal environment.
Release notes
For questions, contact: arc-sra-team@mail.nasa.gov