NASA NTRS · 19940032407
An arbitrary grid CFD algorithm for configuration aerodynamics analysis. Volume 1: Theory and validations
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.
Keep this discovery
Explore connections, maps & timelines
Baker, A. J., Iannelli, G. S., Manhardt, Paul D., Orzechowski, J. A.. 1993-12-01. An arbitrary grid CFD algorithm for configuration aerodynamics analysis. Volume 1: Theory and validations. https://ntrs.nasa.gov/citations/19940032407
Cite the original work for its findings. Save a collection to share your selection of sources.