Arush Kumar Singh

Hi, According to my understanding: In the CEA paper: https://ntrs.nasa.gov/api/citations/19950013764/downloads/19950013764.pdf page 25 section 4.1 there is a line "For each species heats of formation (and, when applicable, heats of transition)...

Hi NJC, For map correction, u can read: https://ntrs.nasa.gov/api/citations/20070018165/downloads/20070018165.pdf For solver convergence, you can read: https://openmdao.github.io/PracticalMDO/Notebooks/Homeworks/Problems/debug_solvers.html Basically, by changing the initial value for the off-design condition, the code wouldn't throw...

Can you please be more specific? We run the design analysis to fix the geometry of the engine. And then run the off design to match this geometry. So, we...

In the nozzle module, the throat area is defined as an output. So you have to add the reverse equations in the nozzle module, or somehow try to bypass the...

Did you pull the latest changes from pycyle. This bug was solved in PR #103

This is an addon file that you can use to check the error between the two solution methods. i.e CEA and tabular. Yeah, this file might cause confusion in the...

The input of compressor map is Wc(mass flow corrected), PR(pressure ratio) and efficiency. We need two points to get any point on the map and they could be PR and...

You can input any another map from your side, u can call the functions plot_compressor_maps, plot_turbine_maps from viewer.py to plot your maps.

What is the new reasoning structure? How do I add it in the args?