Final answer:
The low-flying aircraft P is traveling at a constant speed of 360 km/h in the holding circle of radius 3 km. The angular speed of the aircraft can be calculated using the formula ω = v / r, where v is the linear speed of the aircraft and r is the radius of the holding circle.
Step-by-step explanation:
The low-flying aircraft P is traveling at a constant speed of 360 km/h in the holding circle of radius 3 km.
To find the quantities r, r', r'', θ, θ', and θ'', we need more information about the specific positions and velocities of the aircraft at those instants. However, we can calculate the angular speed ω of the aircraft using the formula ω = v / r, where v is the linear speed of the aircraft and r is the radius of the holding circle. In this case, ω = 360 km/h / 3 km = 120 rad/h.