- #1
Hornbein
- 2,700
- 2,250
I'm interested in the very basics of drag, both for ships in water and airplanes in air. Here's what I have so far :
Flow of the medium can be laminar or turbulent. As the relative speed of the vessel increases, the more likely the flow is to be turbulent.
Laminar drag increases linearly with speed.
Turbulent drag increases exponentially with speed.
Drag depends linearly on the surface area, all other things being equal.
For a large airplane about half of the energy goes into drag, the rest being the energy needed to provide lift.
Questions : Would it be reasonable to assume that turbulent drag increases with the square of the speed? If not, what are the values for water and air?
How does drag depend on the density of the medium?
How does drag depend on the mass of the boundary layer?
For a Boeing 787, at what airspeed does turbulent flow begin?
For a modern cargo ship, at what speed does turbulent flow begin?
I will be making very rough approximations so subtleties don't matter all that much. I want to keep it very simple.
Flow of the medium can be laminar or turbulent. As the relative speed of the vessel increases, the more likely the flow is to be turbulent.
Laminar drag increases linearly with speed.
Turbulent drag increases exponentially with speed.
Drag depends linearly on the surface area, all other things being equal.
For a large airplane about half of the energy goes into drag, the rest being the energy needed to provide lift.
Questions : Would it be reasonable to assume that turbulent drag increases with the square of the speed? If not, what are the values for water and air?
How does drag depend on the density of the medium?
How does drag depend on the mass of the boundary layer?
For a Boeing 787, at what airspeed does turbulent flow begin?
For a modern cargo ship, at what speed does turbulent flow begin?
I will be making very rough approximations so subtleties don't matter all that much. I want to keep it very simple.