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Idea - FICS

Aerodynamic Design, Performance Characterization and Drogue Trajectory Analysis of a Wing-Mounted Aerial Refueling System for a Fighter Aircraft

Team and Contact Details

Student Name School Degree Year Email
MUHAMMAD SHAHEERCAEUndergraduateFourth[email protected]
MUHAMMAD SHAHEERCAEUndergraduateFourth[email protected]

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Idea Details

Idea Name: Aerodynamic Design, Performance Characterization and Drogue Trajectory Analysis of a Wing-Mounted Aerial Refueling System for a Fighter Aircraft
Slogan: Aerodynamic Design, Performance Characterization
Supervisor Name: Dr Omer Khan
Supervisor Designation: Professor
Supervisor School: CAE
Supervisor Department: CAE
Contact number: 0320-3761371
Email ID: [email protected]
Abstract:
    In this research thesis aerodynamic effects of an external modification in shape of probe and drogue wing-mounted aerial refueling system on a fighter jet aircraft configuration will be characterized. Aerodynamic design and integration of the aerial refueling probe with the aircraft will be carried out using computer aided design tools. Variations in aircraft aerodynamic behavior between original
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Status: new
Entry Date & Time: 2023-02-08 (1908)