5.101: PROBLEM DEFINITION
Situation:
A hovercraft is supported by air pressure.
l=15ft,w=7ft,W=2000lbf,
Find:
Air flow rate necessary to support the hovercraft.
Assumptions:
Air is incompressible.
Steady flow.
Viscous effects are negligible.
Air in the chamber is at stagnation conditions (V=0,p=uniform)
Just under the skirt p=patm
Properties:
Air (T=60◦F,p=1atm),ρ=0.00237 slug/ft3,Table A.3.
PLAN
Because flow rate is the goal, apply Q=VA.The steps are:
1. Find the pressure in the chamber by apply force equilibrium in the vertical direc-
tion.
SOLUTION
1. Force equilibrium (vertical direction)
2. Bernoulli equation (elevations terms are neglected; point 1 is in the chamber; point
2 is underneath the skirt)
3. Flow rate equation