22.2.4 Scalar and Vector quantities

22.2.4 Differentiate between scalar and vector quantities; and
(a) explain and or apply vector addition and subtraction;
(b) demonstrate understanding and ability to resolve vector diagrams or problems.

Different between…

Scalar : is just a magnitude, “Speed”  or Distance etc.

 Wind Speed is…?

Vector : (Velocity) Has both a “Direction” and “Speed”. 

Wind Velocity is Direction / Speed

(a) an examples of doing additions (+) with vectors

With a simple Scalar examples….

Adding VectorsVector-1 is right 6 units+ Vector-2 is right 2 units= resultant of right 8 units

Subtracting VectorsVector-1 is right 8 units+ Vector-2 is left 2 units= resultant of right 6 units

These examples here is a Aircraft  Air Speed (black line) and the wind speed (blue line) equals the  Aircraft Ground Speed(red line)

Adding vector quantities.

Nose to Tail VectorsVector-1+ Vector-2= resultant

This examples here is a Aircraft ‘s Heading and Air Speed (black line).  

The wind’s Direction and Speed (blue line),

 equals the  Aircraft’s Track across the ground and Ground Speed(red line)

To resolve vector each vector needs to be  head to tail  and in scale

Vector Diagram showing the wind Triangle.

(b) resolving vector diagrams.

Resolving a Vector into componentscomponent-1component-2Vector

Resultant Force , resolved into “Lift” and “Drag”

 We often use these vectors to explain modes of flight

 straight and level, turning, navigation, etc

Thus an easy way for us to explain and resolve forces (draw up and see what actually going on),

                    

                        

Sweep-Back / Lateral Stability

Sweep-back:

Sweep-Back helps with lateral stability,

Sweep-Back and lateral movement causes a different change in aspect ratio of each wing,

that create the correcting roll to slow/stop the lateral movement

Sweepback refers to the angle at which an aircraft’s wing is set back from a right angle to the body. Sweepback helps the aircraft gain lateral stability, therefore righting it if it is disturbed in roll. 

Dihedral

sweepback

In the diagram, you can see that when an aircraft rolls and slips, the relative airflow doesn’t meet the aircraft directly head on. This means, the effective span, and therefore the aspect ratio of each wing is different. 

Aspect ratio = span / mean chord line

This means, the lower wing has a higher aspect ratio, and therefore produces more lift, this in turn raises the lower wing back to straight and level. 

22.2.2 Units of measurement. State;

22.2.2

 

Why do we need to have an understanding of aeroscience:

To achieve a constant and clear understanding of aviation science and flight measurement, it is important to be familiar with accepted aviation units of measurements.

 

Units of measurement. State;

(a) the International System (SI) units for length, mass, time and temperature (°K and °C);

Length: metre (m)

Mass: kilogram (kg)

Time: seconds (s)

Temperature: degrees Celsius (°C) / Kelvin (°K)  (0°C = 273°K)

 

(b) the derivation of the SI units for force, pressure, power, and the non-SI units;

Force: newton (N)

Pressure: pascal (Pa)

Power: watt (W)

 

(c) Altitude, navigation distance and speed;  /??/  (c) foot, nautical mile, knot and horsepower.

Altitude: feet (ft)

Navigation distance: nautical miles (nm)

Speed: Knots (kt)

These units of measurement are used throughout our study of Principles of Flight

the factors affecting centripetal force and rate of turn.

xSpeed² / ÷Radius Fast

Slow

.

Blue Line is: According to Newton’s first law, an object in motion will remain in motion in a straight line unless acted upon by an external force. 

In an aircraft turn, the centrifugal force acts to pull the aircraft toward from the center of the turn, The amount is shown by length of the arrows.

In simple terms, more you need to defect from the straight path the more force required.

The speed and radius of an aircraft in a turn both have a significant effect on the aircraft’s performance.

Speed: In general, the faster an aircraft is traveling, the more energy it has and the greater the forces acting on it during a turn. Higher speed can result in higher lift and g-forces, which can cause the aircraft to bank more steeply and turn more tightly. However, if the speed is too high, the aircraft may not be able to maintain control and could stall.

Radius: The radius of a turn is determined by the angle of bank and the speed of the aircraft. A smaller radius of turn requires a steeper bank angle and a higher g-force, which can put stress on the aircraft and its occupants. A larger radius of turn requires a shallower bank angle and a lower g-force, which is less demanding on the aircraft but takes longer to complete the turn.

Overall, the speed and radius of a turn are interdependent and must be carefully managed by the pilot to ensure safe and efficient flight. The aircraft’s performance characteristics, such as its weight, wing loading, and stability, also play a role in determining the speed and radius of a turn.

..

CPF=m x v2 / r 

CPF=mass x velocity2/ radius 

CPF= Wv2/g ‘r’

                                      Image result for ball on a string centripetal force gravity

So, we can see that the strength of our centripetal force, depends on the mass of our object (heavier it is the more force is required to keep it on our curved flight path) the velocity (faster it’s flying the harder it is to keep on our curved flight path) and the radius of the circle (a tighter circle / shorter distance will require more force to keep it on the flight path)

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