https://github.com/bergercookie/turbomachines-project
Python Code for Turbomachines Course
https://github.com/bergercookie/turbomachines-project
Last synced: about 1 year ago
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Python Code for Turbomachines Course
- Host: GitHub
- URL: https://github.com/bergercookie/turbomachines-project
- Owner: bergercookie
- Created: 2014-02-22T09:33:33.000Z (over 12 years ago)
- Default Branch: master
- Last Pushed: 2014-07-14T20:56:30.000Z (almost 12 years ago)
- Last Synced: 2025-02-12T23:45:49.999Z (over 1 year ago)
- Language: Python
- Homepage:
- Size: 506 KB
- Stars: 0
- Watchers: 3
- Forks: 0
- Open Issues: 0
-
Metadata Files:
- Readme: README.md
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README
**Homework on Turbomachines, 5th semester, National Technical University of Athens**
************************************************************************************
Sat Feb 22 11:49:38 EET 2014, nickkouk
Problem Set:
=============
Problem 1:
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1-D mathematical analysis of an axial turbine
1. find 6 pairs of phi-psi points for 3 given efficient rates: htt = 0.9, 0.925, 0.95
2. find the maximum efficient rate for the current circumstances: r -> known
Problem 2:
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Was implemented solely on paper so there is no code written for it
Problem 3:
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1-D analysis of a 7-stage compressor
1. Calculate the thermodynamic properties and the velocities (absolute & relative) of every single position,
3 positions at each stage. 1-entrance to rotor, 2-after the rotor,
before the stator, after the stator (beginning of next stage)
Also calculate the losses of every stage
2. Calculate the polytropic & isentropic efficient rates of every rotor & stage of the compressor
Also calculate the exponential of the polytropic process of every rotor & stage
3. Print out nicely each one of those values