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Exam (elaborations)

CPAER GENERAL KNOWLEDGE - SHARPER EDGE

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CPAER GENERAL KNOWLEDGE - SHARPER EDGE

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CPAER GENERAL
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CPAER GENERAL









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Institution
CPAER GENERAL
Course
CPAER GENERAL

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Uploaded on
August 15, 2024
Number of pages
9
Written in
2024/2025
Type
Exam (elaborations)
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CPAER GENERAL KNOWLEDGE - SHARPER EDGE
Chord - Answers -Straight line joining leading edge to the trailing edge

Camber line - Answers -Line which runs midway between upper and lower surfaces of
the airfoil joint the trailing and leading edge.

Camber - Answers -The measure of the curvature of the airfoil.

Expressed as a percentage

Angle of attack - Answers -The angle between the chord of the wing and the relative
airflow

Centre of pressure - Answers -Lift and drag act through the centre of pressure of the
wing. The centre of pressure moves with a change in the angle of attack.

Centre of gravity - Answers -The point through which the resultant of the weight of all of
the components on the aircraft can be considered to act.

The centre of ____ is ahead of the centre of _____. - Answers -Gravity, pressure.

Axes of rotation - Answers -Three axes which rotate about the aircrafts centre of gravity

Lateral axis associated with... - Answers -Pitch

Longitudinal axis associated with... - Answers -Roll

Vertical axis associated with.... - Answers -Yaw

Lift acts... - Answers -Perpendicular to relative airflow

Weight acts... - Answers -Towards the centre of earth (gravity)

Thrust acts... - Answers -Along the longitudinal axis in the direction of motion

Drag acts... - Answers -Parallel to relative airflow

Aspect ratio - Answers -The measure of the slenderness of a wing.

The ratio of the wing span to the wing chord.

Wings with a ___ aspect ratio are more efficient and aerodynamic. Why? - Answers -
High because they produce less induced drag.

.

, Induced at low.

When is drag the least? - Answers -Middle of the speed range. This is known as Vmd
(minimum drag speed)

Which type of drag changes with angle of attack? - Answers -Induced.

Drag and an increase in altitude... - Answers -Induced drag increases.

Parasite drag decreases.

Drag and aircraft weight... - Answers -Induced drag increases.

Parasite remains the same.

Drag and speeds... - Answers -Induced is highest at low speed and lowest at high
speeds.

Parasite is lowest at low speeds and highest at high speeds,

Ground effect - Answers -Induced drag is significantly reduced.

Wing tip vortices are also greatly reduced.

Ground effect will be greater on aircraft with... - Answers -Low wings and short landing
gear.

____ acts through the centre of gravity and ____ acts through the centre of pressure. -
Answers -Weight.

Lift.

The centre of ____ must always be in front of the centre of _____. - Answers -Gravity.

Pressure.

The further the distance between the two centres (forward c of g).... - Answers -The
larger nose down pitching moment, resulting in the requirement of more downwards
force created by the tail section decreasing performance due to an increase of induced
drag.

Maximum range - Answers -Maximizing the distance flown per unit of fuel.

Piston engines aircraft: speed for best lift to drag ratio.

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