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If an aircraft is descending and thrust is added, but no other control inputs are changed, what will be the result?
When flap is added to a descending aircraft and airspeed is maintained with a constant power setting:
Flap is used for landing because it:
Later in your studies, increased power will become a factor in using flaps for approach. Jet engines take time to spool up at low thrust settings so a high power setting is preferred to reduced to spool up time.
Later in your studies, increased power will become a factor in using flaps for approach. Jet engines take time to spool up at low thrust settings so a high power setting is preferred to reduced to spool up time.
A headwind while descending to land in a glide approach will make the aircrafts:
An aircraft is descending with a tail wind. For any given constant settings, will the aircraft land longer down the runway or shorter on the runway, compared to an approach with no wind, in the exact same configuration?
Two identical aircraft are landing in a rough formation, one aircraft is 200 kg heavier than the other. Is it possible that they can attain the same glide ratio?
It is angle of attack that determines glide ratio. So as long as the heavier aircraft flies faster to maintain the same angle of attack, the glide ratio can be the same.
It is angle of attack that determines glide ratio. So as long as the heavier aircraft flies faster to maintain the same angle of attack, the glide ratio can be the same.
Power plus attitude determines performance in:
A aircraft with a stall speed of 45 knots is approaching in a headwind of 20 knots, at an IAS of 55 knots. The gusty headwind suddenly reduces to 5 knots. What is the likely outcome?
With a reduction of 15 kts HW, the IAS will now be 40 kts. This is below the stall speed.
With a reduction of 15 kts HW, the IAS will now be 40 kts. This is below the stall speed.
If an aircraft is descending on a 5 mile final and hits wind shear, where it goes from 20 knot headwind to 30 knots, but maintains its nose attitude, the aircraft will in the long term:
With the onset of more headwind, the descent angle will be steeper. The aircraft will require more power in the long term to maintain the optimum descent path.
With the initial sudden gust of headwind, the aircraft will be high of profile. If that headwind is maintained, the aircraft will land shorter if the pilot maintains IAS / nose attitude as its speed over the ground will be less for the same rate of descent.
With the onset of more headwind, the descent angle will be steeper. The aircraft will require more power in the long term to maintain the optimum descent path.
With the initial sudden gust of headwind, the aircraft will be high of profile. If that headwind is maintained, the aircraft will land shorter if the pilot maintains IAS / nose attitude as its speed over the ground will be less for the same rate of descent.
Wind shear that causes an aircraft to lose height is called what type of shear?
RPL Aerodynamics Exam Progress
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