Aerodynamics Flashcards

1
Q

What do Vortex Generators do?

A

The provide air flow control that delays boundary layer separation by energizing the air.

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2
Q

What two factors affect lift in a turn?

A

Angle of attack and airspeed

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3
Q

What is the advantage of a swept wing aircraft?

A

Higher critical mach speed

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4
Q

What effect does altitude have on mach number?

A

Mach number increases as altitude increases

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5
Q

What effect does altitude have on stall speed?

A

TAS stall speed increases with altitude.

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6
Q

What causes an aircraft to hydroplane the most?

A

Under inflated tires.

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7
Q

How does CG effect range and stability?

A

Rearward CG increases range and stability

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8
Q

Why is the critical mach lower at higher altitudes?

A

The speed of sound is lower

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9
Q

What effects specific range?

A

Gross weight, altitude, aircraft configuration

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10
Q

Why does specific range increase with increase in altitude?

A

Greater TAS, lower air temperature, increased engine RPM, lower fuel consumption

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11
Q

What is the effect of cargo shifted from a forward compartment to an aft compartment?

A

Less stability and higher cruise speed.

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12
Q

What determines the optimum cruise altitude for a jet?

A

Gross weight at the beginning of cruise.

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13
Q

What is the disadvantage of a swept wing design?

A

Dutch roll tendency, wing tip stalls first, reduced max coefficient of lift.

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14
Q

What are the effects of a forward CG?

A

Increased stability (longer moment arm from CG to tail), lower cruise speed (more downforce from tail required), Higher stall speed (stalling angle of attack reached at a higher speed), greater elevator back pressure (more airflow required over the elevator), Good stall recovery

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15
Q

What are the effects of a rearward CG?

A

Decreased longitudinal stability, Higher cruise speed, Lower stall speed (less wing loading), Poor stall recovery

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