Help me understand wing loading

There is probably some up/down force, but a fuselage is a very inefficient airfoil shape (very, very low aspect ratio if nothing else) and would create a lot of drag relative to the lift. So you would want to minimize that factor by pretty much lining up the fuselage with the airflow.

Look at the glide angle of lifting body aircraft...

Or the Shorts 3-30/3-60 where the fuselage contributed a small but significant portion of total lift. Somewhere between 13% and 19% (I think) I don't recall the exact number. At least that is what they taught us in ground school. But that was 1988 and that is a long time ago.
 
You created goalposts out of thin air. If you started out level, which is What the scenario was, then you must remain level in order to have the load factor be 1.41. Nobody would assume you were starting out descending and then banked and continued to descend at the same rate. That’s nonsense that you made up so you can say you were right. The premise is that you started level. If you don’t stay level and bank, and allow the plane to descend naturally, it will increase its descent rate and will Never have a load factor of 1.41.

It’s way past time for you to give it up.
 

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There is probably some up/down force, but a fuselage is a very inefficient airfoil shape (very, very low aspect ratio if nothing else) and would create a lot of drag relative to the lift. So you would want to minimize that factor by pretty much lining up the fuselage with the airflow.

Look at the glide angle of lifting body aircraft...
The Piaggio P.180 Avanti is the only production [now former production] plane that has a "lifting body" fuselage.
 
Most people would assume that you were level to begin with. If you were going to assume otherwise, it should have been stated.
So your entire argument is based on an assumption that your psychic powers tell you is valid?
 
Most people would assume that you were level to begin with. If you were going to assume otherwise, it should have been stated.

Who was "level to begin with"? Who or what are you talking about?

In Post 4 I made a statement of fact. No assumptions are required.
 
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Who was "level to begin with"? Who or what are you talking about?

In Post 4 I made a statement of fact. No assumptions are required.
In post 4 you made a statement of fact that the turn does not have to be level. But it has to be something. Your earlier statement, "Load factor in a 45 degree bank turn is 1.41," is incomplete. Load factor in some 45 degree banked turns in 1.41. One of the conditions that makes that true is a coordinated level turn. So you are indeed making assumptions. And you're attacking someone for making different assumptions.
 
In post 4 you made a statement of fact that the turn does not have to be level. But it has to be something. Your earlier statement, "Load factor in a 45 degree bank turn is 1.41," is incomplete. Load factor in some 45 degree banked turns in 1.41. One of the conditions that makes that true is a coordinated level turn. So you are indeed making assumptions. And you're attacking someone for making different assumptions.

I have spent 3 pages defending Post 4, not Post 2.
 
The load in a 45-degree turn is the square root of two times what it would be in a zero degree turn. Is that good enough. It doesn't require any more qualification.

The turn "factor" is an indication that this is a dimension less number, so you its applied between two values of similar dimensions.

Wing loading is weight over /area.
 
The load in a 45-degree turn is the square root of two times what it would be in a zero degree turn. Is that good enough. It doesn't require any more qualification.

The turn "factor" is an indication that this is a dimension less number, so you its applied between two values of similar dimensions.

Wing loading is weight over /area.
Sure. But, it’s worth understanding that you can avoid that increased load if you let the nose drop.
 
Sure. But, it’s worth understanding that you can avoid that increased load if you let the nose drop.

Everyone understands that the elevator controls G load. I don't know why this thread is still going.
 
Sure. But, it’s worth understanding that you can avoid that increased load if you let the nose drop.
But that's not what load factor is. It's sort of like saying, I can lose weight just by sitting in a chair if I stop eating.

But what is worth NOTING is that the force on the plane is not decreased just because you descend. You must be accelerating downward (the drastic case is the "0g pushover"). The plane will not sustain a reduction in load for very long.
 
I will stop trying to have any conversation beyond what you two think are important on this thread since apparently you are the only ones allowed to make a point on the thread. Good day. What I am saying is not wrong. It’s just not what you want to say, so enjoy your echo chamber.
 
I will stop trying to have any conversation beyond what you two think are important on this thread since apparently you are the only ones allowed to make a point on the thread. Good day. What I am saying is not wrong. It’s just not what you want to say, so enjoy your echo chamber.
I lost track in the back and forths what you mean to say, actually. Are you saying that a turning glider has less 'g's than a power plane, since it's always descending (even when rising in an air bubble)? Or that a 60° banked spiral has less than two 'g's? Do you think "unloading" the wing to prevent stalling when turning final will still allow you to roll out lined up with the runway? None of those are true.
 
I lost track in the back and forths what you mean to say, actually. Are you saying that a turning glider has less 'g's than a power plane, since it's always descending (even when rising in an air bubble)? Or that a 60° banked spiral has less than two 'g's? Do you think "unloading" the wing to prevent stalling when turning final will still allow you to roll out lined up with the runway? None of those are true.
Here’s his original post, and it seems to still be his position...
It does to have the 1.41 load factor. The load factor only occurs if you remain level. If you allow the nose to drop as much as it wants to naturally, then load factor is 1, but you’ll be in a pretty brisk decent. If you allow the nose to drop but not all the way, you still won’t get 1.41 load factor, but something between 1 and 1.41.
 
The statement is still wrong. The "nose dropping as much as it wants naturally" is completely meaningless. Whether the nose will drop at all depends on how the plane is trimmed. The only way you're going to get a load factor of 1 in a 45-degree bank is to be accelerating the plane downward at a rate of at least .4 g's. Not just descending, not just pitched over, it's go to be "light in your seat" downward acceleration.
 
I will stop trying to have any conversation beyond what you two think are important on this thread since apparently you are the only ones allowed to make a point on the thread. Good day. What I am saying is not wrong. It’s just not what you want to say, so enjoy your echo chamber.

Dude, your first two sentences in post #8 are flat wrong, which started all this. All your nonsense tap dancing and arguing doesn't change that, but being wrong in public is the highest form of butthurt I guess.
 
The statement is still wrong. The "nose dropping as much as it wants naturally" is completely meaningless. Whether the nose will drop at all depends on how the plane is trimmed. The only way you're going to get a load factor of 1 in a 45-degree bank is to be accelerating the plane downward at a rate of at least .4 g's. Not just descending, not just pitched over, it's go to be "light in your seat" downward acceleration.
If anyone doubst this, they should take a bathroom scale and find an elevator, preferably a fast express elevator, and stand on that scale and see what it says at rest, when the elevator starts and stops both upward and downward, and during a steady rate of ascent or descent. I haven't done it but I sure know that once that elevator has established its climb or descent I sure don't weigh any more or less.
 
If anyone doubst this, they should take a bathroom scale and find an elevator, preferably a fast express elevator, and stand on that scale and see what it says at rest, when the elevator starts and stops both upward and downward, and during a steady rate of ascent or descent. I haven't done it but I sure know that once that elevator has established its climb or descent I sure don't weigh any more or less.
That fact was never in dispute by me.
 
That fact was never in dispute by me.
“Only” seems to me like it disputes it pretty well.
It does to have the 1.41 load factor. The load factor only occurs if you remain level. If you allow the nose to drop as much as it wants to naturally, then load factor is 1, but you’ll be in a pretty brisk decent. If you allow the nose to drop but not all the way, you still won’t get 1.41 load factor, but something between 1 and 1.41.
 
“Only” seems to me like it disputes it pretty well.
Good lord. I shouldn’t have said never, yes, that was inaccurate, and I admitted as much over a day ago.
 
So, if you’re not remaining level (or ascending), where is the Increased load coming from?
Student pilot here..... But does centrifical force have any thing to do with weight /wing loading ?
As a kid after milking a cow and packing the milk bucket to the house .... I'd swing the bucket over my head in a windmill fashion. Never spilled the milk . (Well ok once while learning to ). It seemed the bucket gained weight in relation to hanging straight down . Could do the same swinging it horizontal while turning around and around .
Would it not be same with wing loading in a turn ?
 
Student pilot here..... But does centrifical force have any thing to do with weight /wing loading ?
As a kid after milking a cow and packing the milk bucket to the house .... I'd swing the bucket over my head in a windmill fashion. Never spilled the milk . (Well ok once while learning to ). It seemed the bucket gained weight in relation to hanging straight down . Could do the same swinging it horizontal while turning around and around .
Would it not be same with wing loading in a turn ?

Other than there is no such thing as "centrifical[sic] force" and you are describing "load factor"(wing loading is something else), yes. The actual force applied(by your arm in case of milk, by part of wing's lift in case of plane) is Centripetal Force. Which is the force that needs to be applied to the object to overcome its inertia(commonly perceived as "centrifugal force") in order to make it travel in a curve
 
Student pilot here..... But does centrifical force have any thing to do with weight /wing loading ?
As a kid after milking a cow and packing the milk bucket to the house .... I'd swing the bucket over my head in a windmill fashion. Never spilled the milk . (Well ok once while learning to ). It seemed the bucket gained weight in relation to hanging straight down . Could do the same swinging it horizontal while turning around and around .
Would it not be same with wing loading in a turn ?
Yes, and you can break off the wings by loading them with forces, whatever those forces are named.
 
But does centrifical force have any thing to do with weight /wing loading ?
Not really. The "load" on the wing is 100% due to aerodynamics forces and 0% due to gravity and centripetal acceleration. What happens when you let go of the rope? The aerodynamic forces are the equivalent of the rope except that they depend only on what you do with the yoke.

Lettuce conduct some thought experiments.

You are flying along straight and level - you feel 1g under your butt, your wings are providing lift equal to the weight of the aircraft. Now, all of a sudden, Congress repeals the laws of gravity. What happens? Your lift doesn't go away, the "upward" force that had been balancing the acceleration of gravity now accelerates you upward. You still have 1G under your butt. Eliminating gravity did not change the loading on the wings - it just changed the trajectory of the aircraft. (You end up in a continuous loop...)

On the other hand, you are again flying on straight and level. Someone accidentally pulls the plug and all of the Earth's atmosphere suddenly wooshes down the drain and you are surrounded by vacuum. Now you have no lift from the wings (you can simulate the same effect by ejecting your wings in flight if you want to try this yourself). The "loading" is zero. The force under your butt is zero. No lift, no drag. Gravity is accelerating the airplane, it's contents, and you downwards at 32.2 ft/sec^2. You are in free fall.

External forces from things like gravity and centripital acceleration affect your trajectory, but do not result in loading of the wings - take them away and the load remains the same. The forces that you measure / feel / load the wings come strictly from the aerodynamic forces which are 100% controlled by the pilot. If you want a load of 1.414 g, you don't bank at 45 degrees, you pull back until you get 1.414g. Now, as part of our training, we learn to automatically pull as we roll to maintain altitude - it becomes a trained reflex (or muscle memory if you prefer), so it seems like the loading goes up in a turn. But that is just us, as pilots, making it happen even if we are no longer really aware that we are doing it.
 
Sorry Geoff, I don't buy your first analogy. If gravity were to go to zero, wing loading would cease to exist. Wing loading is defined as weight over area. Weight is the mass of the airplane times the gravitational accelleration (1g). In 0g, the weight is 0, and the wing loading is zero.

Further, you'd feel it. You're now accelerating upward and you'd fell that quiet easily.
 
Sorry Geoff, I don't buy your first analogy. If gravity were to go to zero, wing loading would cease to exist. Wing loading is defined as weight over area. Weight is the mass of the airplane times the gravitational accelleration (1g). In 0g, the weight is 0, and the wing loading is zero.

Further, you'd feel it. You're now accelerating upward and you'd fell that quiet easily.
If you accelerated upward at 9.8 meters per second per second and there was no gravity it would feel the same as if there was gravity. The force you feel from gravity feEls as if it is pushing down. The force you would feel from accelerating upwards in the absence of gravity would also feel like it's pushing down. The vectors are different but what you feel (momentum or resistance to) is the same.
 
If the law of gravity was repealed the air would instantly decompress as fast as its mass would allow and you wouldn't get much lift at all in any direction after about three seconds.
:)
 
External forces from things like gravity and centripital acceleration affect your trajectory, but do not result in loading of the wings

Loading the wings results in centripetal acceleration does it not? Just because the causality runs a certain direction, doesn't mean they have nothing to do with each other.
 
So Ryan ol' buddy.....how's this thread workin' out for ya? ;)

I've wondered the same thing and after reading this thread and specifically the posts of the two people who actually attempted to answer your question, sounds like "wing loading" is just an engineer's way of saying that if your plane is heavy, you have a higher wing load. Light? Less wing load.
 
wing loading would cease to exist.
Lift is 1/2 * density * velocity squared * coefficient of lift. Erasing gravity won't change any of those numbers. The lift generated by the wing moving through the air will be the same. Since gravity is pulling your butt down at 32.2 ft/sec^2 the wing (in level flight) is generating enough lift to counteract that. Turn off gravity, lift doesn't change, now you are accelerating your butt upward at 32.3 ft/sec^2. If you had your eyes closed, you would never feel the difference.

Further, you'd feel it. You're now accelerating upward and you'd fell that quiet easily.
Essentially, you are claiming that the observation that Einstein made that lead him to the General Theory of Relativity is incorrect...
 
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sounds like "wing loading" is just an engineer's was of saying that if your plane is heavy, you have a higher wing load. Light? Less wing load.
yup. The published wing loading is a number on a piece of paper that you can use to compare one airplane to another. Has nothing to do with anything that happens in flight.
 
Loading the wings results in centripetal acceleration does it not? Just because the causality runs a certain direction, doesn't mean they have nothing to do with each other.
The causality happens because of what the pilot does. Changing gravity (if that were possible) would not change the lift without the pilot (or trim) changing the angle of attack in response.
 
Depends on which way the wing is pointing.
If you are "banked" some of the lift is pointed in towards the center of a circle, so it results in centripetal acceleration. How much depends on the bank angle and how hard you pull. If you pull (push) to a zero g loading, there is no centripetal acceleration.

Centripetal acceleration doesn't have to be horizontal.
 
Lettuce conduct some thought experiments.

You are flying along straight and level - you feel 1g under your butt, your wings are providing lift equal to the weight of the aircraft. Now, all of a sudden, Congress repeals the laws of gravity. What happens? Your lift doesn't go away, the "upward" force that had been balancing the acceleration of gravity now accelerates you upward. You still have 1G under your butt. Eliminating gravity did not change the loading on the wings - it just changed the trajectory of the aircraft. (You end up in a continuous loop...)
Whell, my thought experiment crashed and I need search and rescue.

In my scenario I was flying a perfectly round loop de loop, floating over the top with zero 'g' each time around with a consistent three 'g' at the very bottom. When congress repealed the law of gravity, exempting congressional members and the air the gas bags breathe, I noticed I then had gained one 'g' on the top and lost one at the bottom. As my speed stabilized at a new constant value, which before was twice as fast at the bottom, I realized the 'g' load was settling down between one and two 'g's. Your thought experiment says I should only have one 'g' all the way around. Mine was higher. Centrifugal force?
 
In my scenario I was flying a perfectly round loop de loop, floating over the top with zero 'g' each time around with a consistent three 'g' at the very bottom.
So you were slower on the up line faster on the down line because of gravity and had to change your pull on the top and bottom to compensate. With gravity off, you would no longer have the speed changes and making the loop round would involve sitting there with the stick in one position. You could pick any G load you wish.
 
So you were slower on the up line faster on the down line because of gravity and had to change your pull on the top and bottom to compensate. With gravity off, you would no longer have the speed changes and making the loop round would involve sitting there with the stick in one position. You could pick any G load you wish.
Ah, I think I see. If I would have been equipped with auto-throttles for maintaining a constant airspeed and been trimmed hands off my 'g' load at the bottom might have been, say, two 'g's with zero at the top prior to the repeal, and one and one after, just like you predicted! Thank you!
 
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