NASA NTRS · 19940032415
An arbitrary grid CFD algorithm for configuration aerodynamics analysis. Volume 2: FEMNAS user guide
Abstract
This report documents the user input and output data requirements for the FEMNAS finite element Navier-Stokes code for real-gas simulations of external aerodynamics flowfields. This code was developed for the configuration aerodynamics branch of NASA ARC, under SBIR Phase 2 contract NAS2-124568 by Computational Mechanics Corporation (COMCO). This report is in two volumes. Volume 1 contains the theory for the derived finite element algorithm and describes the test cases used to validate the computer program described in the Volume 2 user guide.
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Manhardt, Paul D., Orzechowski, J. A., Baker, A. J.. 1992-09-01. An arbitrary grid CFD algorithm for configuration aerodynamics analysis. Volume 2: FEMNAS user guide. https://ntrs.nasa.gov/citations/19940032415
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