Runway Design — Required Takeoff Speed and Runway Length
Question: You are designing an airport for small planes. One kind of airplane that might use this airfield must reach a speed before takeoff of at least v and can accelerate at a constant rate of a.
(a) If the runway is 150 m long, can this airplane reach the required speed for takeoff?
(b) If not, what minimum length must the runway have?
Note: The numerical values of the required speed and acceleration are missing from the supplied question, so the solution below is expressed in terms of v and a.
Given Information
Initial speed: u = 0 m/s
Required takeoff speed: v m/s
Constant acceleration: a m/s²
Available runway length: s = 150 m
Method 1: Use the Third Equation of Motion
Since the airplane starts from rest and accelerates uniformly, use the equation that connects velocity, acceleration, and displacement without requiring time:
v² = u² + 2as
Since u = 0:
The minimum runway length needed to reach takeoff speed v is:
smin = v² 2a
Compare this required length with the available 150 m.
Case 1: If v²/(2a) ≤ 150, the airplane can reach the required takeoff speed within the runway.
Case 2: If v²/(2a) > 150, the runway is too short. The minimum required runway length is v²/(2a).
Part (a): Can It Take Off Within 150 m?
Find the maximum speed the airplane can reach over 150 m. Use:
vmax² = 2a(150)
vmax² = 300a
vmax = √(300a)
Compare this speed with the required takeoff speed v.
If √(300a) ≥ v, the airplane can reach takeoff speed in 150 m.
If √(300a) < v, it cannot reach the required speed in 150 m.
Part (b): Minimum Runway Length
The airplane must accelerate from rest to the required takeoff speed v. From:
Rearranging:
smin = v² 2a
Substitute the numerical takeoff speed and acceleration from the complete textbook question to obtain the runway length in metres.
Alternate Method 2: Use Average Velocity
For constant acceleration, the average velocity is:
Since the airplane starts from rest, u = 0:
Distance travelled equals average velocity multiplied by time:
s = vavgt
s = vt/2
Using v = at, the time to reach the takeoff speed is:
Substitute into the distance equation:
s = v 2 × v a
s = v²/(2a)
This gives the same minimum runway length as Method 1.
Alternate Method 3: Use the Time Equation First
First calculate how long the airplane needs to reach takeoff speed:
Since u = 0:
Then use the displacement equation:
Since u = 0:
s = ½at²
s = ½a(v/a)²
s = v²/(2a)
Final Results
Maximum speed over 150 m: vmax = √(300a)
Can the plane take off? Yes, if √(300a) ≥ v; otherwise, no.
Minimum runway length: smin = v²/(2a)