Misc Aerody. Flashcards

1
Q

Best Endurance is achieved by flying at the A??

A

AOA which yields minimum fuel flow per hour.

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2
Q

Best Endurance occurs at a speed for Vimd and at an altitude where Vimd can be achieved using engine .. .. ..

A

design RPM

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3
Q

Wind has NO EFFECT on endurance because.. .. ..

A

fuel flow per hour is unaffected by wind!

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4
Q

As FOB is burnt, weight reduces, the drag curve moves down and left resulting in

A

LOWER maximum endurance speeds at LOWER Gross Weights!

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5
Q

The AOA for best endurance is

A

FIXED!

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6
Q

The speed for best endurance is dependant on w & a

A

Weight and Altitude!

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7
Q

(climbing)

Max AOC is achieved by flying at V?

A

Vimd

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8
Q

As weight reduces the curve moves down and left resulting in lower ….

A

Excess thrust speeds at lower gross weights!

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9
Q

AOA for max AOC is fixed but the speed depends on W & A

A

Weight and Altitude

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10
Q

Max ROC achieved using max

A

Power

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11
Q

Power available is developed by multiplying thrust by T….

A

TAS

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12
Q

Power available at Zero TAS is…

A

ZERO –> and increases as TAS increases.

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13
Q

Flaps increase lift and drag moving the curve up and….

A

LEFT

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14
Q

As flaps are lower Vimd

A

decreases!

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15
Q

Power available decrease with altitude. TAS or max ROC is higher with increased altitude but the IAS is….l

A

Lower!

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16
Q

It is common to climb at fixed IAS (increasing TAS) to about FL250 then at cons….

A

constant MACH which results in decreasing TAS and IAS (speed protection)

17
Q

In a constant MACH climb the reduction of IAS compared to TAS

A

is much greater but ROC remains reasonable constant!

18
Q

Approach attitude with leading edge devices only is h…

A

Higher

19
Q

Approach attitude with trailing edge devices only is l…

A

Lower

20
Q

Approach attitude with leading and trailing edge devices only is …

A

medium (just right)

21
Q

Long Range Cruise tables publish speeds for lower gross weights to conserve

A

AOA!

22
Q

Long Range Cruise speeds are typically 5% faster than Maximum Range Cruise speed and results in only a _ %

A

1% reduction in range!

LRC=99% of max range speed!

23
Q

Max Thrust reduced with increases in

A

Altitude,
Temperature,
Humidity!

24
Q

Thrust decreases until the aircraft approaches the speed of its exhaust, at high speeds some thrust is ‘recovered’ due to R.E>

A

Ram Effect - the increase of Mass Air Flow as a result of air being compressed at the intake at high speed.

25
Q

Temperature rise due to the compression of air limits the benefit of Ram….rec…

A

Ram Recovery!

26
Q

Flying at the speed of your exhaust achieves 100% propulsive efficiency but produces ZERO th…

A

Zero Thrust!