NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
An arbitrary grid CFD algorithm for configuration aerodynamics analysis. Volume 2: FEMNAS user guideThis 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.
Document ID
19940032415
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Manhardt, Paul D.
(Computational Mechanics Co. Knoxville, TN, United States)
Orzechowski, J. A.
(Computational Mechanics Co. Knoxville, TN, United States)
Baker, A. J.
(Computational Mechanics Co. Knoxville, TN, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Subject Category
Computer Programming And Software
Report/Patent Number
NAS 1.26:196135
NASA-CR-196135
CMC-TR4.2-92-VOL-2
Report Number: NAS 1.26:196135
Report Number: NASA-CR-196135
Report Number: CMC-TR4.2-92-VOL-2
Accession Number
94N36922
Funding Number(s)
CONTRACT_GRANT: NAS2-12568
CONTRACT_GRANT: SBIR-02.07-5494
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available