Propeller windmilling, the truth

Interesting discussion topic.

On a twin screw ship with controllable pitch propellers, with one engine making way and the other engine shut down, you go much faster with the dead engine free spinning like ‘windmilling’ airplane propeller than when the shaft is locked. We don’t have an option to feather the prop.

So why would an airplane propeller be opposite?
The different viscosity of water and air, perhaps? Also, do you leave the spinning propeller turning the diesel engine (or steam turbine in an older ship), or do you declutch it so that it's just the prop spinning? If you could declutch an airplane propeller from the engine, the drag from windmilling would be negligible.
 
Yes, there is some momentum in the prop which takes energy to sustain, but the helicopter is a bad example because the larger disk and weight (though lesser RPM) than an airplane propeller.
 
Interesting discussion topic.

On a twin screw ship with controllable pitch propellers, with one engine making way and the other engine shut down, you go much faster with the dead engine free spinning like ‘windmilling’ airplane propeller than when the shaft is locked. We don’t have an option to feather the prop.

So why would an airplane propeller be opposite?
A thin, compressible medium versus a viscous, incompressible medium, with the blades on the former a tiny fraction of the relative area of the blades on the latter?
 
If you could declutch an airplane propeller from the engine, the drag from windmilling would be negligible.

Unfortunately this not correct. Even if your engine breaks right at the propellor shaft, that windmilling propellor if it stayed attached will be a giant air brake.
 
As pointed out in Post # 14, Fig 15 may infer the logic: It all depends on the propeller pitch. At below about 40° AoA, the power required to windmill rises dramatically. If the prop loses its low pitch stop, I'd suspect the "disk theory" is real, but I'll defer to an aerodynamicist. :)

Windmilling prop.JPG
 
A rather silly discussion. Not much you can do about it on a fixed prop. Here's a good question for everyone. If you're trying to stop the prop to extend your glide you likely haven't got a workable engine. My question is without oil pressure can you feather a complex prop?

Depends on the plane.
 
A rather silly discussion. Not much you can do about it on a fixed prop. Here's a good question for everyone. If you're trying to stop the prop to extend your glide you likely haven't got a workable engine. My question is without oil pressure can you feather a complex prop?
If it's a single engine piston with a hydraulic governor, no. You'll need oil pressure.

But if it's got an electrically controlled prop, then you're in luck.
 
If it's a single engine piston with a hydraulic governor, no. You'll need oil pressure.

But if it's got an electrically controlled prop, then you're in luck.


Some twins are also supposed to go auto-feather upon oil pressure loss.
 
If it's a single engine piston with a hydraulic governor, no. You'll need oil pressure.

But if it's got an electrically controlled prop, then you're in luck.
There are springs to pull the prop blades to a default position, which the governor pulls it away from:
  • in piston singles, the spring pulls the blades towards flat pitch (high RPM, opposite of feathered), so that a governor failure won't kill your only engine
  • in piston twins, the spring pulls towards coarse pitch, so that they will feather by default if there's a failure
Lots more in this classic article: https://www.avweb.com/features_old/pelicans-perch-16those-marvelous-props/
 
The physics guys/gals will tell you that work is force X velocity. No rotation means no work (turning the engine). Yes, there will be drag as the prop is being pushed through the air.

The smarter ones will tell you that work is force x distance rather than velocity. If you try to calculate force using velocity you will have The Force, and it will be with you, always.
 
The smarter ones will tell you that work is force x distance rather than velocity. If you try to calculate force using velocity you will have The Force, and it will be with you, always.
I thought we were trying to calculate work.
 
I think the discussion has now achieved flight radius of a swallow level…..

http://style.org/unladenswallow/


Estimating the Airspeed Velocity of an Unladen Swallow

By Jonathan Corum

Nov. 17, 2003

After spending some time last month trying to develop alternate graphic presentations for kinematic ratios in winged flight, I decided to try to answer one of the timeless questions of science: just what is the airspeed velocity of an unladen swallow?

What do you mean, an African or European Swallow?
To begin with, I needed basic kinematic data on African and European swallow species.

Although 47 of the 74 worldwide swallow species are found in Africa,1 only two species are named after the continent: the West African Swallow (Hirundo domicella) and the South African Swallow (Hirundo spilodera), also known as the South African Cave Swallow.

Since the range of the South African Swallow extends only as far north as Zaire,............................
 
I know not everyone is a fan of this, but I practice both pulling the throttle to idle, as well as completely shutting the engine off:

https://www.pilotsofamerica.com/community/threads/engine-out-practice.124291/

If you practice both ways, you'll have a feel for how your plane actually (not just theoretically) performs.
If you do it often enough and if the real situation ever occurs, you'll have a decent idea of what your glide will look like, which, at the end of the day is what really matters.
 
As pointed out in Post # 14, Fig 15 may infer the logic: It all depends on the propeller pitch. At below about 40° AoA, the power required to windmill rises dramatically. If the prop loses its low pitch stop, I'd suspect the "disk theory" is real, but I'll defer to an aerodynamicist. :)

It can be computed to be a disk of "some size" but the "size of the prop arc" is nonsense. Aerodynamicists talk about an equivalent "flat plate area" but they don't mean that's necessarily equivalent to size of the prop arc.
 
It can be computed to be a disk of "some size" but the "size of the prop arc" is nonsense. Aerodynamicists talk about an equivalent "flat plate area" but they don't mean that's necessarily equivalent to size of the prop arc.
So then, it could even be more than the the flat plate of the prop arc? :eek:
 
The different viscosity of water and air, perhaps? Also, do you leave the spinning propeller turning the diesel engine (or steam turbine in an older ship), or do you declutch it so that it's just the prop spinning? If you could declutch an airplane propeller from the engine, the drag from windmilling would be negligible.
I think this is wrong. I think the whole “turning the engine requires work therefore it causes more drag” is wrong. It’s very easy to increase drag without producing any “work”. I don’t think the engine rotating is relevant. But this whole subject has always been a mystery to me so I admit I might be totally wrong.
 
It’s very easy to increase drag without producing any “work”.
Not if you're using the PHYSICS definitions of those words. Drag is a force. That drag acting through a displacement is work.
 
Not if you're using the PHYSICS definitions of those words. Drag is a force. That drag acting through a displacement is work.
I can create drag without resulting in any parts moving. Ie like a rotating an engine, but yes, technically you are correct, drag is a force.
 
I think this is wrong. I think the whole “turning the engine requires work therefore it causes more drag” is wrong. It’s very easy to increase drag without producing any “work”. I don’t think the engine rotating is relevant. But this whole subject has always been a mystery to me so I admit I might be totally wrong.
Work is the amount of energy transferred by a force acting through a distance. If the aircraft is moving through the air, then the drag force is causing the aircraft to do work on (i.e., transfer energy to) the air. If the propeller is turning a dead engine, then the propeller is doing work on (i.e., transferring energy to) the engine. Assuming a dead engine, that energy in both cases is ultimately coming out of gravitational potential energy, so if a constant glide speed is maintained, then the total rate of energy transfer dictates the rate of descent.
 
Not all inoperable engines will drag the same either:
-out of fuel, engine (prop) otherwise spinable
-broken internal parts, spins but engine gonna drag a lot and create more damage and either increase or decrease drag over time
-broken internal parts, locked up/seized, prop fixed in place (no windmilling possible).

Now I don’t know how much torque a prop being pushed through the air at 100 kts will create, so not sure how seized a seized engine needs to be for a prop to not turn.
 
I'm not a physicist, so I'm sure there's a flaw in my logic that someone will point out, but if it took less energy for the prop to be stopped than spinning, wouldn't the prop stop on its own?
The propeller is designed to convert the relative wind to rotational velocity in most circumstances. The energy comes ultimately from gravity. What you want to do is convert as much of that energy as possible to lift rather than drag.
 
Unfortunately this not correct. Even if your engine breaks right at the propellor shaft, that windmilling propellor if it stayed attached will be a giant air brake.
Yes, a free-spinning propeller would still provide some drag even if it weren't turning an engine, but the drag would be considerably less.

The information everyone wants is in NACA report 464 "NEGATIVE THRUST AND TORQUE CHARACTERISTICS OF AN ADJUSTABLE-PITCH METAL PROPELLER" (from way back in the 1930s) which examined this question in detail. Here is the resulting drag at 75 mph for the different configurations tested (the table contains other wind speeds as well):

Propeller stopped:
17° pitch: 53.0 lb drag
80° pitch (feathered): 3.3 lb drag

Propeller spinning (17° pitch):
Free spinning: 33.7 lb drag
Turning a stopped engine: 68.6 lb drag
Engine at idle (power for 350 rpm): 60 lb drag

One important point here is that the stopped, unfeathered propeller is producing almost as much drag as the one that's still windmilling and driving the engine, so it's really not worth pulling the plane almost into a stall to stop the prop for extra gliding range.
 
The NACA data also suggests why the glide range is improved when the prop control is pulled out in a plane with a controllable pitch propeller. Singles are typically not featherable, but it at least gets you part of the way there.
 
When a helicopter engine quits the pilot selects a flat pitch and rotor blades continue turning .... which causes so much drag (large disc) the machine descends to the ground about the speed of a descending parachute.

Don't forget that in any unpowered rotating airfoil (propeller, rotor blade, prop-rotor) there are driving and driven regions.

That means the rotating airfoils are also producing lift from the driven region. Propellers are no different.
 
This thread reminds me of this clip from "and justice for all":


It's about 10 minutes, but the first 3:30 are the relevant bits.

...and IK04's timing is perfect.
 
I've always thought about this the same way I do about helicopters. No engine and stop the rotor and it drops like a rock. Let the air turn the rotor and you descend at a reasonable rate.

Granted an airplane propeller is quite a bit smaller, but the principle should be the same.
 
I've always thought about this the same way I do about helicopters. No engine and stop the rotor and it drops like a rock. Let the air turn the rotor and you descend at a reasonable rate.

Granted an airplane propeller is quite a bit smaller, but the principle should be the same.
That’s the one that convinces me without a doubt that windmilling is more drag, but that doesn’t mean it’s the engine rotating that’s the main factor.
 
That’s the one that convinces me without a doubt that windmilling is more drag, but that doesn’t mean it’s the engine rotating that’s the main factor.
No need to guess any more — see my earlier post quoting the NACA report. https://www.pilotsofamerica.com/com...dmilling-the-truth.132499/page-2#post-3132908

In their test, with a 75 mph relative wind, a free-spinning prop produced 33.7 lb of drag in their configuration; a windmilling propeller turning a dead engine produced 68.6 lb of drag.

The big surprise for me was that an unfeathered, stopped propeller created far more drag than the free-spinning one — 53.0 lb vs 33.7 lb. Water and air are very different, but that might answer the earlier questions about why you leave a ship's propeller spinning (presumably unclutched from the engine) when one of the engines fails, rather than stopping it. In this case, the drag from the unfeathered airplane propeller increased by >40% when they stopped it rather than just letting it spin freely, disconnected from the engine.
 
Last edited:
Here is the resulting drag at 75 mph for the different configurations tested

65 Knots? That is barely relevant to most planes that people are flying where best glide speeds are much higher than that. Drag is exponential, not linear with wind speed.
 
No need to guess any more — see my earlier post quoting the NACA report. https://www.pilotsofamerica.com/com...dmilling-the-truth.132499/page-2#post-3132908

In their test, with a 75 mph relative wind, a free-spinning prop produced 33.7 lb of drag in their configuration; a windmilling propeller turning a dead engine produced 68.6 lb of drag.

The big surprise for me was that an unfeathered, stopped propeller created far more drag than the free-spinning one
65 Knots? That is barely relevant to most planes that people are flying where best glide speeds are much higher than that. Drag is exponential, not linear with wind speed.
Yeah but that just means that the numbers would be bigger at higher speed. Until you reached a point where compressibility became a factor I don’t think the relationships in the 75 knit data would change. But I’m not an engineer. Where is @nauga and company to weigh in on this one?
 
Water and air are very different, but that might answer the earlier questions about why you leave a ship's propeller spinning (presumably unclutched from the engine) when one of the engines fails, rather than stopping it. In this case, the drag from the unfeathered airplane propeller increased by >40% when they stopped it rather than just letting it spin freely, disconnected from the engine.

There is a huge difference between a ship's prop and an aircraft propeller. The blades of a prop on a large ship cover about 75% of the area of the circle. Typical single engine airplane propeller is probably only about 5%.
 
65 Knots? That is barely relevant to most planes that people are flying where best glide speeds are much higher than that. Drag is exponential, not linear with wind speed.
I chose 75 mph because I assumed that was more typical of the glide speed for an airplane at the time (1930s), but as I mentioned, the report measured at 25 mph, 50 mph, 75 mph, and 100 mph. The numbers for 100 mph are higher, but their relationships are the same:

Propeller stopped:
17° pitch: 94.4 lb drag
80° pitch (feathered): 5.8 lb drag

Propeller spinning (17° pitch):
Free spinning: 60.1 lb drag
Turning a stopped engine: 101.0 lb drag
Engine at idle (power for 350 rpm): 100.0 lb drag

The windmilling propeller now (turning the engine) is still producing much more drag than a free-spinning one, and a stopped propeller is producing almost as much drag as a windmilling one. Feel free to read the original NACA 464 report for details: https://digital.library.unt.edu/ark:/67531/metadc66121/m2/1/high_res_d/19930091538.pdf
 
There is a huge difference between a ship's prop and an aircraft propeller. The blades of a prop on a large ship cover about 75% of the area of the circle. Typical single engine airplane propeller is probably only about 5%.
Since even the smaller wetted area of the airplane propeller stopped caused far more drag than the airplane propeller spinning free (declutched from the engine), I'd think that would apply even more so to the ship's propeller.
 
Sailboats have small diminutive propellers, when we used to race we'd always leave the motor in gear to prevent the prop from spinning. Hearing that whine of the spinning prop was an indication that it was slowing us down

But a sailboat propeller is not a ship propeller, and we did eventually upgrade to a folding propeller
 
Since even the smaller wetted area of the airplane propeller stopped caused far more drag than the airplane propeller spinning free (declutched from the engine), I'd think that would apply even more so to the ship's propeller.
That the document you reference is from the 1930's does not necessarily mean it's valid. There are a lot of things that were accepted as gospel at the time which are now proven to be incorrect. I recall that cigarette smoking was considered a treatment for asthma at one time.
 
So, I need to read the linked docs still, been traveling, but here’s where I lose it. If turning the engine is what causes the drag, then why is it so hard to stop the engine from turning? I stalled the plane and still couldn’t stop the windmilling in a skycatcher with the engine not running. If it’s causing so much drag, why won’t it stop spinning?
 
Back
Top