The Bede BD-5J is a small single seater airplane powered by the Jet Engine, The following...

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The Bede BD-5J is a small single seater airplane powered by the Jet Engine, The following are the specifications of the aircraft: Wing Span: 5.18 m Wing Planform Area: 3.51 m² Gross Takeoff Mass: 435.5 Kg Fuel Capacity: 210 Liters (Density of Fuel = 0.804 kg/l at 15°C) Power Plant: Micro Turbojet TRS 18 (Max. Thrust at Sea Level = 900 N, Specific Fuel Consumption of 0.6 kg/(kg.hr) Drag Polar Equation of the Aircraft is given by. Cp = 0.02 +0.062C Cruise Speed: 369 kmph Stall Speed: 89 kmph, Maximum Speed: 373 kmph Question No 2: Plot the Thrust required and Thrust available curves for the Bede BD-5J Aircraft at sea level and Calculate the Rate of Climb at the Cruise Speed The Bede BD-5J is a small single seater airplane powered by the Jet Engine, The following are the specifications of the aircraft: Wing Span: 5.18 m Wing Planform Area: 3.51 m² Gross Takeoff Mass: 435.5 Kg Fuel Capacity: 210 Liters (Density of Fuel = 0.804 kg/l at 15°C) Power Plant: Micro Turbojet TRS 18 (Max. Thrust at Sea Level = 900 N, Specific Fuel Consumption of 0.6 kg/(kg.hr) Drag Polar Equation of the Aircraft is given by. Cp = 0.02 +0.062C Cruise Speed: 369 kmph Stall Speed: 89 kmph, Maximum Speed: 373 kmph Question No 2: Plot the Thrust required and Thrust available curves for the Bede BD-5J Aircraft at sea level and Calculate the Rate of Climb at the Cruise Speed

Answer rating: 100% (QA)

Certainly Lets go through the calculations Step 1 Calculate the drag coefficient CD at the cruise sp... View the full answer