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The lift of an aircraft is directly proportional to the
- a)Speed of aircraft
- b)Square of the speed of aircraft
- c)Does not depend on speed
- d)None of the above
Correct answer is option 'B'. Can you explain this answer?
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Verified Answer
The lift of an aircraft is directly proportional to thea)Speed of airc...
Lift opposes the downward force of weight, is produced by the dynamic effect of the air acting on the airfoil and acts perpendicular to the flightpath through the center of lift. The lift generated by
An airfoil depends on such factors as:
• Speed between airflow and aircraft (v)
• Density of the air
• Total area of the segment or airfoil (A)
• Angle of attack (AOA) between the air and the airfoil
CL is the lift coefficient at the desired angle of attack, Mach number, and Reynolds number.
• Speed between airflow and aircraft (v)
• Density of the air
• Total area of the segment or airfoil (A)
• Angle of attack (AOA) between the air and the airfoil
CL is the lift coefficient at the desired angle of attack, Mach number, and Reynolds number.
Most Upvoted Answer
The lift of an aircraft is directly proportional to thea)Speed of airc...
Lift opposes the downward force of weight, is produced by the dynamic effect of the air acting on the airfoil and acts perpendicular to the flightpath through the center of lift. The lift generated by
An airfoil depends on such factors as:
• Speed between airflow and aircraft (v)
• Density of the air
• Total area of the segment or airfoil (A)
• Angle of attack (AOA) between the air and the airfoil
CL is the lift coefficient at the desired angle of attack, Mach number, and Reynolds number.
• Speed between airflow and aircraft (v)
• Density of the air
• Total area of the segment or airfoil (A)
• Angle of attack (AOA) between the air and the airfoil
CL is the lift coefficient at the desired angle of attack, Mach number, and Reynolds number.
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The lift of an aircraft is directly proportional to thea)Speed of aircraftb)Square of the speed of aircraftc)Does not depend on speedd)None of the aboveCorrect answer is option 'B'. Can you explain this answer?
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