Can an Aerospace Engineering Student Be Expelled for Fabricating Gas Turbine Thrust and SFC Logs?

A university will summarily expel an aerospace or aeronautical engineering undergraduate, cancel all aircraft propulsion and gas turbine laboratory credits, and report the student to the Council for the Regulation of Engineering in Nigeria (COREN) for professional debarment for fabricating jet engine gas turbine thrust output measurements, faking turbine inlet temperatures ($TIT$), or forging thrust specific fuel consumption ($TSFC$) calculations without operating physical propulsion test stands. In aerospace engineering curricula accredited by COREN, aircraft propulsion testing—including running micro-turbojet engines or turbofan simulators on instrumented thrust test stands, measuring load cell thrust force in newtons, recording fuel mass flow rates, and evaluating compressor pressure ratios—represents a life-critical flight safety competency; fabricating jet propulsion data subverts aircraft performance calculations, conceals dangerous turbine blade thermal fatigue risks, and violates professional engineering ethics.

Departmental laboratory coordinators and propulsion testing examiners utilize digital engine control data acquisition logs to detect fabricated experimental submissions.

1. The aerospace propulsion course lecturer audits submitted practical portfolios and identifies mathematically idealized Brayton cycle thermal efficiency curves that ignore compressor boundary-layer aerodynamic losses.
2. The chief laboratory technologist checks the gas turbine propulsion testing bay sign-in register and confirms that the student never signed out turbojet test stands, Jet-A1 aviation fuel, or optical pyrometers.
3. The technologist checks the test cell acoustic control console logs and confirms that no turbine engine runs were executed during the student’s claimed testing hours.
4. The student is formally issued an academic query requiring them to perform a live jet engine start cycle on a micro-turbine and demonstrate turbine inlet temperature monitoring.
5. Inability to explain gas turbine starting sequences or replicate thrust calculations leads to a formal charge of scientific fabrication and academic fraud.
6. The Head of Department transmits an investigative dossier to the Faculty of Engineering Board and the University Central Student Disciplinary Committee (SDC).
7. The student appears before the disciplinary committee to defend their submissions under constitutional principles of fair hearing.
8. The University Senate considers the committee’s findings and ratifies an order of rustication or summary expulsion, notifying COREN to bar future professional licensure.

Acquiring hands-on competency in aircraft propulsion testing is essential for aerospace engineers who will design, test, and maintain commercial jet engines, military aircraft propulsion systems, and aerospace rockets.

• Standardized aircraft propulsion laboratory manual with approved gas turbine testing protocols.
• Raw bench workbook recording shaft RPM, thrust force (N), fuel flow rates, turbine inlet temperatures, and exhaust gas velocities.
• Gas turbine test cell sign-in register confirming equipment allocation and jet fuel consumption.
• Plotted engine performance curves displaying thrust and thrust specific fuel consumption versus turbine shaft speed.

Students must record actual experimental measurements honestly, accounting for ambient air density and humidity variations, rather than manufacturing idealized propulsion data.

Under COREN professional regulations and university examination codes, fabricating aircraft propulsion testing data is classified as severe academic fraud, carrying mandatory expulsion and total debarment from the aerospace engineering profession nationwide.

Maintaining rigorous laboratory ethics ensures that aerospace engineering diplomates and graduates develop sound technical judgement required to design and operate safe, reliable aircraft propulsion systems.