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Flow-Past-Through-Submerged-Body

Given: Military aircraft with M=8000 kg, lands on 350 km/hr and is slowed by a parachute with `A=10 m^2` area. Find

Estimate time needed to slow to 200 km/hr.

Maximum deceleration rate.
Model chute as an open hemisphere. [2070-Chaitra ][8]

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Similar Question

This Chapter Flow-Past-Through-Submerged-Body consists of the following topics

A jet plane having a wing area of `30 m^2` and weighing 28 KN flies at 900 km/hr. The engine develops 8000 KW and has a mechanical efficiency of 70%. Determine the lift and drag coefficient for the wind taking density of air as 1.2 kg/`m^3`.

Given: Military aircraft with M=8000 kg, lands on 350 km/hr and is slowed by a parachute with `A=10 m^2` area. Find

Estimate time needed to slow to 200 km/hr.

Maximum deceleration rate.
Model chute as an open hemisphere.

A kite has an effective area of `0.6 m^2` and mass 0.4 kg. It experience a drag of 15 N in a wind speed of 40 km/hr. Determine
the tension in the chord if it makes an angle of `45^0` with the horizontal.

lift coefficient for the kite
Consider the density of air as 1.2 kg/`m^3`.

Given: Military aircraft with M=8000 kg

lands on 350 km/hr and is slowed by a parachute with `A=10 m^2` area. Find Estimate the time needed to slow to 200 km/hr. Maximum deceleration rate. Model the chute as an open hemisphere.

Flow Past Through Submerged Body

Fluid-Mechanics