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Evaluation of Fuel Consumption of B747-400 in Short-range Flight with Catapult Assist

  • Lee, Changhyeok (Div. of Aerospace, Automotive and Mechanical Engineering of Dong Seoul University) ;
  • Park, Hyunchul (Div. of Aerospace, Automotive and Mechanical Engineering of Dong Seoul University)
  • Received : 2020.05.29
  • Accepted : 2020.07.07
  • Published : 2020.08.31

Abstract

Recently, the aviation industry has sought to reduce its carbon usage in aircraft operations. Specifically, the industry is proceeding with the development of ultra-large turbofan engines and the development of hybrid electric engines to reduce the fuel consumption of aircraft. In one case, Airbus is developing as its future goal an aircraft with a short take-off distance that uses a catapult. In this study, when a b747-400 aircraft with two of the four engines removed was tested using a catapult, its fuel consumption was compared with that of the original aircraft. Fuel consumption was calculated using the mass flow consumption formula. Further, the aircraft L/D ratio caused by engine removal was interpreted using the CFD Tool, Ansys Fluent. The results showed that the lift ratio was improved by about 7% and that the fuel efficiency was improved by about 14%.

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