Whole aircraft drag Flashcards

1
Q

What is induced drag

A

Caused by vortices which occur whenever lift is produced.

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2
Q

What is total drag

A

Total drag is the sum of all drag
Subdivided into Induced drag(lift)
and parasite drag which occurs regardless of lift.

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3
Q

What is interference drag

A

Aircraft surface presented at differing angles to relative airflow. Direction of flow differs over theses components. Where these meet different flow velocities meet and local airflow loses energy.

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4
Q

What can form by interference drag

A

Some junctions boundary layer gets thicker and slows causing separation while at others vortices can for due to high energy air flows meeting at an angle.

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5
Q

What factors affect form drag.

A

Greater the airspeed greater the form drag. Pressure on front surfaces greater than rear surfaces resulting in greater net force acting backwards on the object.

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6
Q

What affects form drag

A

Kinetic energy of boundary layer.

Amount of streamlining aft of point of thickness.

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7
Q

What are the influencing factors on skin friction drag

A

Speed-high shear forces leading to greater skin friction drag.
Surface area- larger surface area means S more skin friction drag.
Boundary layer-turbulent boundary layer more skin friction drag
Surface roughness-turbulent boundary layer.

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8
Q

Does parasite drag change

A

Once design of plane is complete many elements of parasite drag become fixed.

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9
Q

Relationship between speed and parasite drag

A

Parasite drag increases as the square of speed. Eg is speed doubles parasite drag increase fourfold

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10
Q

Influence of flaps on parasite drag

A

Increasing frontal are increases parasite drag. When flaps or landing gear is deployed parasite drag curve becomes steeper

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11
Q

Parasite drag Equation

A

0.5x rho xV2 x S xCdp
Parasite drag is proportional to air speed squared
Aircrafts surface area
Coefficient of parasite drag.

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12
Q

What is the coefficient of parasite drag determined by

A

Aircrafts shape and amount of streamlining.
Surface roughness.
Presence and effectiveness of fillets.

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13
Q

What influences induced drag

A

Vortices and downwash are primary cause of induced drag.

Anything that affects intensity of vortices affects amount of drag.

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14
Q

Relationship between speed and induced drag

A

Induced drag is inverse to speed squared.

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15
Q

Relationship between airspeed and weight

A

Heavier aircraft requires more lift to counterbalance weight force.

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16
Q

Relationship between planform and induced drag

A

A wing planform that produces more lift at tips generates more drag

17
Q

Relationship between manoeuvring and induced drag

A

Aircraft manoeuvres by generating more lift force to overcome weight force.. induced drag increases during manoeuvres.

18
Q

Is induced drag proportional or inversely proportional to aspect ratio

A

Inverse Induced drag=1/aspect ratio.

19
Q

What is the coefficient of drag and what are its relationships

A

Cdi is a measure of the downwash or induced AOA.

Cdi is inversely proportional to aspect ratio and directly proportional to lift squared.

20
Q

Equation of induced drag

A

0.5x rho x v2 xS xCdi

21
Q

How can induced drag be reduced

A

Reduced length of tip chord by using high aspect ratio.
Physically restrict movement of air around wing tip i.e winglets
Decrease camber or angle of incidence close to tip.