4 Weeks
Structured learning track with weekly technical progression.
A flagship Dwello program focused on gas turbine engines, turbojet architecture, component flow, performance logic, and guided aircraft engine design.
Structured learning track with weekly technical progression.
Concept sessions, tasks, assignments, and design guidance.
Starts from engine basics and moves toward system-level design thinking.
Final submission focused on designing an aircraft propulsion engine concept.
The program follows the path of air through the engine and explains what each component does to pressure, temperature, velocity, energy, and thrust.
How incoming air is captured, slowed, and delivered to the compressor.
How compressor stages raise pressure and prepare air for combustion.
How fuel-air energy addition increases temperature and gas energy.
How turbine stages extract energy to drive the compressor system.
How exhaust acceleration produces useful propulsive force.
Instead of memorizing component names, students learn why each part exists, how it affects the cycle, and how the complete engine behaves.
Understand engine types, station sequence, airflow path, and the role of each major assembly.
Connect pressure ratio, temperature rise, turbine work, compressor work, and exhaust energy.
Interpret engine performance using thrust, specific fuel consumption, efficiency, and operating conditions.
Learn how supporting systems keep aircraft engines functional, safe, and reliable.
Every Aircraft Propulsion track leads toward designing an aircraft propulsion engine. Longer durations allow deeper calculations, stronger documentation, component sizing, CAD direction, and performance-level detailing.
Students define engine type, airflow path, component roles, basic requirements, and a structured concept-level propulsion design.
Students add cycle logic, pressure-temperature reasoning, performance parameters, station mapping, and stronger design justification.
Students move toward component sizing logic, performance interpretation, system integration, design trade-offs, and detailed technical documentation.
Each week adds one engineering layer: component understanding, cycle logic, performance interpretation, and final engine design documentation.
Engine types, thrust generation, major components, station sequence, airflow path, and propulsion terminology.
Brayton cycle, compressor pressure rise, combustor heat addition, turbine work extraction, and nozzle acceleration.
Thrust, fuel flow, SFC, temperature limits, pressure ratio, efficiency, and operating condition effects.
Students connect component understanding, cycle logic, and performance reasoning into a guided aircraft propulsion engine design output.
The final outcome of the Aircraft Propulsion program is an aircraft engine design output. Students do not stop at definitions or component study — they use the learning to build a structured propulsion engine concept.
As the program duration increases, the intensity of the design increases. A shorter track focuses on conceptual engine design and system understanding, while longer tracks move toward deeper cycle calculations, component sizing logic, performance interpretation, CAD direction, and detailed technical documentation.