An alrcraft has the following relevant specification outlined below: . Weight: 391 kN • Wing planform area: 198 m. • Drag polar: Cp - 0.024 • 0.0870 Engine specific fuel consumption 0.48 b/(bf-hr) Calculate the fuel burn rate las a positive number) when the aircraft is flying in minimum drag conditions at an altitude of 27.248 ft. Give your answer in kilograms per second (kg/s).
An alrcraft has the following relevant specification outlined below: . Weight: 391 kN • Wing planform area: 198 m. • Drag polar: Cp - 0.024 • 0.0870 Engine specific fuel consumption 0.48 b/(bf-hr) Calculate the fuel burn rate las a positive number) when the aircraft is flying in minimum drag conditions at an altitude of 27.248 ft. Give your answer in kilograms per second (kg/s).
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Transcribed Image Text:An aircraft has the following relevant specification outlined below:
Weight: 391 kN
Wing planform area: 198 m.
Drag polar: Cp = 0.024 + 0.087C
· Engine specific fuel consumption: 0.48 lb/lbf-hr)
Calculate the fuel burn rate las a positive number) when the aircraft is flying in minimum drag conditions at an altitude of 27,248 ft. Give your answer in kilograms
per second (kg/s).
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