Minimum Constant Acceleration for Aircraft Liftoff

In summary, to achieve liftoff at a speed of 130km/hr with a run of 271m, the aircraft needs a minimum constant acceleration of 2.41 m/s^2. This can be found by using the equation a=(V^2)/Vi^2 + 2(deltax) and converting the initial velocity of 130 km/hr to 36.11 m/s.
  • #1
delfam
34
0

Homework Statement


aircraft has liftoff speed of 130km/hr. What minimum constant acceleration does it require if the aircraft is to be airborne after a run of 271m? answer is in m/s^2


Homework Equations


V^2 = Vi^2 + 2a(deltax)
a=(V^2)/Vi^2 + 2(deltax)

The Attempt at a Solution


(130^2)/O^2 + 2(271) = a
a = 28.79 km/hr = 230.24 m/s^2
 
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  • #2
The 2nd equation under 2) is not correct. The first equation is ok, so you just need to be careful how you isolate a from it. You should also consider what unit of the values you will use before inserting them (hint: convert km/h to m/s before inserting the value).
 
  • #3
is this right then

(V^2) - (Vi^2)/(deltax) = 2a
 
  • #4
Close. You may mean the right thing, but as you have written it, it misses a set of parenthesis around the the two speeds. Alternatively you can insert vi=0 into the first equation before you start isolating for a.
 
  • #5
so if Vi = 0 then the equation is (V^2)/(deltax) = 2a and 130km/hr = 36.11 m/s so
(36.11 m/s)^2/271m = 2a
4.812 = 2a
a = 2.41 m/s

I feel like i did it right but I need the final units in m/s^2 and isn't this in m^2/s^2
 
  • #6
The square of velocity in unit m/s has unit m2/s2 which then is divided by distance in unit m, so the resulting unit is m/s2 as it should.
 

Related to Minimum Constant Acceleration for Aircraft Liftoff

What is Minimum Constant Acceleration for Aircraft Liftoff?

Minimum Constant Acceleration for Aircraft Liftoff, also known as V1, is the minimum speed at which an aircraft can safely take off and continue the takeoff in the event of an engine failure.

Why is Minimum Constant Acceleration important for aircraft liftoff?

Minimum Constant Acceleration is important because it ensures that an aircraft has enough speed to safely take off and continue the takeoff in the event of an engine failure. It is a critical safety measure for all commercial flights.

How is Minimum Constant Acceleration calculated?

Minimum Constant Acceleration is calculated using a variety of factors, such as the weight of the aircraft, temperature, wind conditions, and runway length. These calculations are done by the pilot and are based on the specific aircraft and flight conditions.

What happens if an aircraft does not reach Minimum Constant Acceleration during takeoff?

If an aircraft does not reach Minimum Constant Acceleration during takeoff, it may not have enough speed to safely continue the takeoff in the event of an engine failure. This can lead to a dangerous situation and potential loss of control of the aircraft.

How does Minimum Constant Acceleration change for different types of aircraft?

Minimum Constant Acceleration can vary for different types of aircraft depending on their size, weight, and engine capabilities. Smaller aircraft may have a lower V1 speed compared to larger aircraft. It is important for pilots to be aware of the specific V1 speed for their aircraft before takeoff.

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