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The ALLSPD-3D Combustor Code is a numerical tool developed by the Internal Fluid Mechanics Division at the NASA Lewis Research Center for simulating chemically reacting flows in aerospace propulsion systems. It provides the designer of advanced engines an analysis tool that employs state-of-the-art computational technology. The code can simulate multi-phase, swirling flows over a wide Mach-number range in combustors of complex geometry.

Current Version:   2.0

License Type:   only for U.S. residents

Home Site:

Source Code Availability:


Available Binary Packages:

  • Debian Package: No
  • RedHat RPM Package: No
  • Other Packages: No

Targeted Platforms:

UNIX. The authors of ALLSPD-3D have not tested it on Linux yet, but they know some Linux users have been successful in running it under Linux. A set of instructions for converting the code to run under Linux is here.

Software/Hardware Requirements:


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