CEP project analyzing a regenerative Brayton cycle for gas turbine power generation. Features intercooling, reheating, regeneration, and EES simulation. Compares ideal (68.9% efficiency) vs real (20.25% efficiency) cycle performance.
Interactive thermodynamics platform for exploring and analyzing power cycles through dynamic diagrams, live simulation, performance calculations, cycle comparison, graphs, optimization, and parametric studies.
Thermodynamic modelling of a gas turbine Brayton cycle using MATLAB to compare constant and temperature-dependent specific heat effects on efficiency and performance.
Package for solving steady state thermodynamic cycles
Interactive 3D operating model of the F-16's GE-F110 turbofan jet engine. Runs in browser.
Gas turbine engine performance from first principles in Python/NumPy: ISA and compressible flow, ideal and real Brayton cycles, a two-spool turbofan, off-design matching (N1, N2, EGT, fuel flow) and trade studies. Validated against closed forms and ICAO/EASA data for the CFM56-7B and LEAP-1B, with a seven-lesson course.
Generic C++/NPSS and MATLAB tool for design and mission performance monitoring of micro turbojet gas turbine engines in UAV applications, benchmarked on the AMT Olympus HP 230N. B.Sc. degree project, IST Islamabad 2025.
Thermodynamic modeling and visual analysis of Ideal Brayton Cycle Thermal Efficiency vs Pressure Ratio across working fluids (Monatomic, Diatomic, Polyatomic).
Simple-cycle gas turbine analyzer in Python with real-fluid properties using CoolProp
Research paper on thermal engineering covering thermodynamic cycles, heat transfer, energy efficiency, Brayton and Carnot cycles, cooling analysis, and sustainable thermal-system design.
Browser-based gas turbine engineering lab: design and off-design cycle analysis, transients, missions, optimization, and uncertainty for turbojets, turbofans, and turboprops.
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