Rotary Flashcards

1
Q

Criteria for Good Airfoil / Rotor Blade? (7)

A
High max static and dynamic lift coefficient
High drag divergence Mach number
Low drag
Low pitching moment
Aft aerodynamic centre position
Sufficient thickness
Easy to manufacture
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2
Q

Coning Angle

A

Is the angle between Tip Path Plane and Blade

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3
Q

Blade Pitch Angle

A

Is the angle between the chord of the airfoil selection and the Plane of Rotation. An increase to Pitch Angle results in an increase to lift.

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4
Q

Angle of Attack

A

Is the angle between the airfoil chord with the direction of the relative wind?

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5
Q

Momentum Theory calculates Thrust (T) directly, where?

A

T = [mass flow per sec] x [total change in velocity]

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6
Q

Using Newton’s 2nd Law and Bernoulli’s Theorem, V2 = 2V1, where V1 is the induced velocity which is axial to the Rotor Disc, and V2 is the induced velocity in the remote wake, also known as?

A

Rotor Downwash

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7
Q

Lift Forces on Blades depends on? (3)

A

Pitch Angle of Blade
Speed of Blade Rotation
Density of Air

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8
Q

Rotor Hinges (3)

A

Flapping Hinge [Vertical]
Feathering Hinge [Horizontal]
Drag Hinge

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9
Q

What is introduced on the main rotor to avoid load variation from root to tip?

A

Blade twist

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10
Q
  • Collective Pitch Lever for ______.
  • Cyclic Pitch Stick for ______, _____ and _____
  • Pedals for ___.
A
  • Collective Pitch Lever for Vertical Movement.
  • Cyclic Pitch Stick for Horizontal Movement, Tilt and Roll
  • Pedals for Yaw.
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11
Q

The limitation to the forward speed of a rotary wing is due to?

A

The blade tip passing into the transonic speed regime, which results in a loss in lift and increases to drag, thus preventing further increases to speed.

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