Engine Cycle Analysis
Well, here I have one of my assignments on Aircraft Engine Analysis which I did in my 3rd Semester of my B.Tech Course. It basically analyses different engines and tries to determine the range of mach numbers for which each engine performs efficiently.
All the animated images shown here are taken from NASA website.
You can download the entire document Engine Analysis.
You can view my code written in C++ to do this assignment source code.
Bondary Layer Analysis
I did this assignment in my 5th sem. This assignment was on finding the numerical solution to the Falkner-Skan transformed u-momentum equation for differnet wedge angles i.e the value of m. It gives the numerical solution to Blasius and Hiemenz equation and also for flow over wedges and corners. The inflection point for negative values of m was also found in this assignment. Post processing was done for each case by finding Boundary layer thickness, Momentum thickness ,Nusselt Number etc. You can download the pdf document as well as the code written in python to do this assignment.
Download:
Boundary_Layer
sourcecode.py
Stability Analysis of CSIR-SARAS aircraft
I did this assignment also in my 5th sem. In this assignment we calculated the stability derivatives for the saras aircraft and did the complete Longitudinal and Lateral Stability Anlysis. We solved the Longitudinal and Lateral equations and found the eigenvalues for both the cases.
Download: Sarasreport.pdf
