Combustion

The Combustion Toolbox for Matlab provides a set of functions for computing basicparameter of gas fuel(density, Wobbe number, combustion velocity, gas mixture parameters, etc.) and gasfuel combustion parameters(combustion air volume, composition, volume and temperature of waste gas, etc.). Platforms: Matlab

Combining the high speed analysis provided by the open source combustion analysis software of catool with the industry leading data aquisition hardware of National Instruments, catoolRT provides a highly powerful yet low cost method of using your existing combustion analysis and data acquisition... Platforms: Windows

HOT is a package originally constructed for combustion modeling in Matlab. It calculates common thermodynamic properties such as enthalpy, specific heat, entropy, internal energy, gamma, ideal gas constant, molecular weight, etc Platforms: Matlab

A comprehensive collection of more than 100 native plug-ins for Adobe After Effects, Apple Final Cut Pro, Autodesk Combustion as well as Boris Red, FX and Graffiti. Final Effects Complete AVX offers a similar collection of native filters for Avid systems. One of the first Adobe After Effects... Platforms: Mac

ShowIEL is a free utility that allows you to view particleIllusion effects. With the new version you can now load any particleIllusion emitter library, including the newer libraries created in particleIllusion 3.0. Version 3.1 now supports ELC files (created with discreet combustion) Although it... Platforms: Mac

Rocket Propulsion Analysis (RPA) is a multi-platform rocket engine analysis tool for rocketry professionals, scientists, students and amateurs. For many years rocketry scientists, students and amateurs were using command-line MS-DOS or UNIX programs to calculate the performance of the rocket... Platforms: Windows

Rocket Propulsion Analysis (RPA) is a multi-platform rocket engine analysis tool for rocketry professionals, scientists, students and amateurs. For many years rocketry scientists, students and amateurs were using command-line MS-DOS or UNIX programs to calculate the performance of the rocket... Platforms: Windows

Given the conditions (Temperature, Pressure, etc.) of the combustion chamber as well as the ambient conditions and the diameter/area of the throat, the program will:a) Solve for the nozzle exit area that produces the max amount of thrust.b) Use the method of characteristics to solve for the shape... Platforms: Matlab