NSAERO |
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The answer to all your fluid flow questions in a single code. Focus on problem solution and not on multiple flow code inputs. Get one software product - NSAERO - for all flow speeds and Reynolds numbers, including gaseous combustion, Rapid problem set up; flexible and general boundary conditions; structured, unstructured and hybrid grids; and many turbulence and chemistry model options give you access to the most complex applications.
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Jet Engine Exhaust Nozzle, Mach Number Contours and Wall Pressure
Distribution Comparison With Experimental Results
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Atmosphere re-entry of a space shuttle with reacting flow.
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OMNI3D, our interactive 3D data visualization tool and TECPLOTTM, the industry standard visualization software, are recommended with NSAERO to give you immediate feedback from results and flexible display of flow properties.
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NSAERO, TECPLOT, and our GridgenTM preprocessing code provide you the ideal software system for fluid dynamics analysis.
TECPLOT is a trademark of Amtec Engineering, Inc., Bellevue, Washington. Gridgen is a trademark of Pointwise, Inc. , Dallas Texas.
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Mach Number and pressure contours for a 3 Elements Airfoil computed with hybrid grids: O-mesh structured grid around the elements and triangulated grid in the surrounding.
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Application Notes |
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System Requirements |
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This software is available for the following systems: irix,linux
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Additional Information |
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