How aircraft fly Flashcards

1
Q

Typical glider ratios

A

17:1 and 20:1 for rigid wings

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2
Q

Is the wind direction of influence for gliders

A

Yes, headwind (wind towards you) can generate more lift

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3
Q

Influence of Wright’s Flyer

A

-first to achieve HtA flight, -dependent on wing warping, which later became ailerons, -highly efficient wings and propellers

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4
Q

Equation of Lift

A

C_L(1/2rhov^2)S

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5
Q

What does the coefficient of lift depend on?

A

On the angle of attack and geometry of the airfoil

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6
Q

Definition of a chord line

A

the line connecting the leading and trailing edge of the airfoil

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7
Q

Definition of a camber line

A

geometric locus of points equidistant between the upper and lower surfaces of the airfoil, mean curvature; influences pressure distribution;

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8
Q

Definition of Angle of Attack

A

the angle between the chord line and the relative wind speed vector

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9
Q

Definition of flaps

A

Trailing edge high-lift devices (increase wing surface area and camber)

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10
Q

Definition of slats

A

Leading edge high-lift devices (increase wing surface area and camber)

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11
Q

What does drag consist of?

A

Profile drag, which includes pressure and friction drag on wings, and parsitic drag (on fuselage)

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12
Q

Piston engine

A

Engine which uses cylinders with 4 cycles

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13
Q

Turbojet

A

Another 4 cycle engine but all stages happen simultanousely

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14
Q

Turbofan

A

Like a turbojet but with bypass air

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15
Q

Turboprop

A

Turbofan but with a propeller

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16
Q

Euler’s equation and the underlying assumptions

A

dp = -rhovdv, gravity is neglected, frictions is neglected, steady flow is assumed, flow may be compressible