rigel09 / compaero Goto Github PK

As the title says, need to put this on PIP.

The current plotting for the Theta Beta Mach plot doesn't work and needs to be fixed.

A good addition to the repo would be to add some more well-thought examples. Perhaps some from a textbook that demonstrates each part of the library.

As the title says. Update all code to PEP8 standards.

• Add a code formatter
• set line length to 100 instead of 80 (80 is annoying short especially with large monitors which are common)
• change all camel case code to snake case

It may be beneficial to add a UI to make the class easier to use if only a simple calculation is needed. The layout would probably be similar to the VT calculator.

Add support for the standard atmosphere tables in the same class-like manner that compressible flow was implemented.

• Add support
• Add tests
• Add documnetation
• Add unit conversions (Maybe its own feature)

Add support for the coefficient of thrust for rocket nozzles.

• Add support
• Add tests
• Add documentation

One of the valid initialization scenarios involves gamma, m2, shock angle, and wedge angle being valid. When implementing this in the UI I noticed that these results were inconsistent. Is it valid that this class can be initialized with that?

Need to finish the implementation for Conical Flows.

• Add Implementation
• Add Tests
• Add some Graphs
• Add Documentation

Add the capability to give each variable as a list or NumPy array to calculate a range of values.

• Add support for feature, while not breaking existing
• Update documentation
• Add tests

Some of the functions dont have any checks regarding input validation. I.E some functions are really only valid if the mach number is greater than 1. Checks need put in place for these functions and tests need to be written for them.

The same value calculated with the option "gamma, Mach" cannot be reduplicated when option "gamma, T/T*" is selected. It seems that the value for T/T* can be calculated from the mach number but the mach number cannot be backed out from that same T/T*.

Steps to reproduce.

1. Go to Fanno Flow Tab in the UI
2. Set Gamma = 1. 4 and Mach = 3 Option = "Gamma, Mach"
3. Calculate
4. Change option to "Gamma, T/T*" and calculate
5. Observe crash.