Straight And Level And Climbing Flight Flashcards

1
Q

Thrust must equal

A

Drag + Wsin0

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2
Q

Lift Must Equal

A

Lift = Wcos0

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3
Q

Steady Climb

A

L = WCOS0
T = D + WSIN0

Weight is greater than lift
Thrust is greater than drag

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4
Q

Descending Flight

A

D = Thrust + Wsin0
L = Wcos0

Weight is greater than lift
Drag is greater than thrust

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5
Q

Maximum Range in glide is obtained by flying at

A

VMD

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6
Q

Mass effect on gliding

A

Glide range independent of mass

Rate of descent - heavy aircraft higher airspeed therefore faster towards ground

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7
Q

Headwind component on climb

A

Increase the flight path angle
Slower ground speed
Same airspeed
Shorter ground distance

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8
Q

Tail wind component on climb

A

Decrease the flight path angle
Greater ground speed
Same air speed
Longer ground distance

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9
Q

Flight path angle

A

Gradient related to ground distance (takes wind into account)

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10
Q

Angle of climb

A

Relative to still air does not take wind into account

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