The Antonov An-225 is the heaviest aircraft ever built, with a maximum takeoff weight of 640 metric tonnes. It also has the largest wingspan of any aircraft in operational service. Sea level standard day (sls) conditions for calculations are 15°C; 101.3kPa Rotate speed (Vr) at takeoff (sls): Vr = 154 kts = 1.2×Vmin (1 kt = 0.514 m/s) Cruise Engine Thrust : a) Calculate the lift coefficient for a standard day takeoff b) Calculate the drag coefficient at cruis Fcruise = 0.85 Fmax Engine maximum thrust: Factual,max = Fsls,max×δ θ½ δ = Pactual/Pref; and θ = Tref/Tactual
The Antonov An-225 is the heaviest aircraft ever built, with a maximum takeoff weight of 640 metric tonnes. It also has the largest wingspan of any aircraft in operational service. Sea level standard day (sls) conditions for calculations are 15°C; 101.3kPa Rotate speed (Vr) at takeoff (sls): Vr = 154 kts = 1.2×Vmin (1 kt = 0.514 m/s) Cruise Engine Thrust : a) Calculate the lift coefficient for a standard day takeoff b) Calculate the drag coefficient at cruis Fcruise = 0.85 Fmax Engine maximum thrust: Factual,max = Fsls,max×δ θ½ δ = Pactual/Pref; and θ = Tref/Tactual
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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The Antonov An-225 is the heaviest aircraft ever built, with a maximum takeoff weight of 640 metric tonnes. It also has the largest wingspan of any aircraft in operational service.
Sea level standard day (sls) conditions for calculations are 15°C; 101.3kPa
Rotate speed (Vr) at takeoff (sls):
Vr = 154 kts = 1.2×Vmin
(1 kt = 0.514 m/s)
Cruise Engine Thrust :
a) Calculate the lift coefficient for a standard day takeoff
b) Calculate the drag coefficient at cruis
Fcruise = 0.85 Fmax
Engine maximum thrust:
Factual,max = Fsls,max×δ θ½
δ = Pactual/Pref; and
θ = Tref/Tactual
![Measurement
A380-800
Wing area
900 m2 (9,680 sq ft)
Maximum take-off weight
640,000 kg (1,400,000 lb)
Operating speed
(800 km/h, 500 mph, 430 knots)
(at cruise altitude)
Cruise altitude
12,500 m (41,000 ft)
Service ceiling
11,000 m (36,000 ft)l254]
Engines (6)
Progress D-18T
Thrust each (at sea level
229.5 kN (51,600 lbf)
standard day)](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F7b4cec44-06d6-4169-a442-5f547cf9543b%2Ff7ae6f71-e6c1-4011-aea8-030afb14d130%2Fdz1g3v_processed.png&w=3840&q=75)
Transcribed Image Text:Measurement
A380-800
Wing area
900 m2 (9,680 sq ft)
Maximum take-off weight
640,000 kg (1,400,000 lb)
Operating speed
(800 km/h, 500 mph, 430 knots)
(at cruise altitude)
Cruise altitude
12,500 m (41,000 ft)
Service ceiling
11,000 m (36,000 ft)l254]
Engines (6)
Progress D-18T
Thrust each (at sea level
229.5 kN (51,600 lbf)
standard day)
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