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Showing 1 to 2 of 2 for “"Panair"”.
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A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows
… flows and 2D shock-expansion theory, and the PANAIR and MARCAP supersonic panel codes. Results correlate well with the analytical solutions, and show strong agreement with the other codes.</p>
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Multi-fidelity analysis and reduced-order modeling of wing-body aerodynamics
Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2024-03-01 without embargo terms