Omar Baaklini

• Developed an engine acceleration method during the takeoff phase, reducing the thrust asymmetry between the two underwing engines from 17% to 1%.

• Conducted in-depth analysis of engine physics and thermodynamics to identify the mechanisms causing the initial thrust difference, using flight simulations.

• Designed and validated a new engine acceleration law, followed by the execution of simulations using an internally developed software.

• Exploited and analyzed the obtained results, demonstrating the near-elimination of the thrust difference between the engines.

• Authored a structured, clear, and detailed technical report, summarizing the methodology, results, and recommendations.