Author Topic: HT, a Question about the Spit FM:  (Read 2530 times)

Offline B@tfinkV

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HT, a Question about the Spit FM:
« Reply #30 on: February 08, 2007, 02:33:18 PM »
problem you are having biggles is flaps, having them deployed at the wrong time will put you in ths spin every time.


flaps are not needed in a spit anywhere as much as youd think when it comes to pucking the nose over in a vertical stall
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Offline Major Biggles

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HT, a Question about the Spit FM:
« Reply #31 on: February 08, 2007, 03:01:49 PM »
Quote
Originally posted by B@tfinkV
problem you are having biggles is flaps, having them deployed at the wrong time will put you in ths spin every time.


flaps are not needed in a spit anywhere as much as youd think when it comes to pucking the nose over in a vertical stall



flaps push you into it more readily, but i was able to put it straight into the stall in the MA, no flaps, you just take it up while slow and cut throttle as you're going over the top

but even if it was only the flaps, it's wrong, and should really be fixed, it's very irritating...

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Offline Stoney74

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HT, a Question about the Spit FM:
« Reply #32 on: February 08, 2007, 03:20:28 PM »
NASA did some testing with spin recovery.  The Grumman AA-1 had a laminar flow wing, and was found to be basically unrecoverable in a fully-developed spin.  Notice the airflow strips on the wings during the spin, and the only solution NASA could come up with to get the plane out of it.

See the video here

Notice that the relative wind as the plane descends does not "push" on the horizontal stab and force the plane nose down, even though I can assure you the plane is nose heavy.  I own and fly one.
« Last Edit: February 08, 2007, 03:24:42 PM by Stoney74 »

Offline airspro

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HT, a Question about the Spit FM:
« Reply #33 on: February 08, 2007, 03:54:53 PM »
Have you tried manual trimming the nose down as much as you can to help get out of your flat spin , stall ?
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Offline Major Biggles

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HT, a Question about the Spit FM:
« Reply #34 on: February 08, 2007, 04:40:14 PM »
stoney, there is no spin, the plane sits still, INVERTED, and floats to the ground. there is no spin, it just sits upside down. no plane falls like a brick upside down, else it would of course be a plane shaped brick, not a combat aircraft...

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Offline Pyro

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HT, a Question about the Spit FM:
« Reply #35 on: February 08, 2007, 08:28:20 PM »
To answer the original question, no it's not intentional.

Offline Kweassa

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HT, a Question about the Spit FM:
« Reply #36 on: February 08, 2007, 08:49:33 PM »
Quote
stoney, there is no spin, the plane sits still, INVERTED, and floats to the ground. there is no spin, it just sits upside down. no plane falls like a brick upside down, else it would of course be a plane shaped brick, not a combat aircraft


 It's the same thing Biggles. What you are arguing about the details is somewhat equivalent of arguing semantics.

 The term 'spin' points out to a plane which enters a state of aggravated stall. The loss of airflow diminishes all normal function of flight surfaces as they cannot effect the attitude of the plane in that state, and the plane starts a spinning momentum initiated by any variety of underlying causes including the angles of each of the roll/pitch/yaw axis, center of gravity, or torque.

 The most frequent state of spin is witnessed when a plane stalls out during a dangerously harsh turn with high AoA and steep bank angle - the ensuing stall dips one of the wings, which subsequently results in a rolling motion while normall airflow is lost over the wings. Hence, the plane shows a continuous spinning motion in the roll axis while it falls nose-down towards the earth. Since in this case, the plane is falling nose down in a favorable AoA to the direction of travel, soon the airflow is somewhat recovered and the aileron starts working again. Thus a plane recovers pretty easily from this state.

 However, in the case of the inverted flat "spin", the stall motion is aggravated as the plane goes belly up, the AoA is completely off from the plane's direction of travel, and soon the elevators and ailerons become useless as the plane starts a slow spin on its yaw axis which is initiated by torque. The stable nature of the plane with a good center of gravity now backfires - and the plane sort of reaches a new "equilibrium" in that new, belly-up state as it starts falling downwards. It effectively becomes a "frisbee".

 The inverted flat spins of AH you mention, is exactly the same thing. Presumably, a slight difference between real life factors and in-game physics is the cause for the minmal difference in attitude. Whereas real-life inverted flat spin would show signs of a true 'spin' as the plane starts rotating on its yaw axis, the AH planes either do not generate enough torque or the momentum caused by the torque is somehow negated, and it falls inverted and flat, but no real sign of spinning motion except a somewhat oscillating motion both in the yaw and pitch axis while it falls flat. However, I personally have experienced a real inverted flat spin in some other planes, so the case might be purely situational.

 The point is this, Major, I've never seen other sim games enter a warplane into a state like this. Others may have witnessed inverted flat spins in AW or WB, but personally, to me AH is the only game I've seen this happen. IL2 has a quite frequent case of normal flat spins in planes such as the P-38, but I've never seen an inverted state of a flat spin there. This "bug" in the flight model you claim, IMO, is actually a testament of how realistic the AH flight model is.


 .....


 One interesting tid-bit, is that there something greatly common with the list of some AH planes that show similar cases of inverted flat spins in the game.

 The Mossie, some Spits, Bf 110, and the P-38s, Ki-84, Ta152 - these are all planes with a relatively large and flat wing/fuselage surface when viewed from top/bottom. Compare the ratio of the wings and the fuselage surface in these planes. All of them have a distinctively large and flat wings, as compared to a short or slender fuselage which is proportionately quite small to the wings. They are all excellent turning planes quite frequently pushed into extremes. They all have great elevator authority which allows them to pull high G turns at speed - which also means can be pushed easily into accelerated stalls by causing a drastic change in AoA while flying at high speed.


 I don't exactly consider it strange to see them entering an inverted flat spin. Most usually these planes try to retain great speeds in the MA, as they are not the 'dragster' type of super planes and the only chance of shooting someone down is by aproaching with speed. Combine that with the fact that they have light elevator authority(except the Ki84) and an inexperienced pilot may very well pull the stick too hard during a steep turn. The AoA will go over its boundaries for normal flight and the plane will stall out. The bank angle is already high since it was in a steep turn - which means a stalling 'wing dip' will cause the plane to go inverted. The AoA freaks out and 'tumbles' the plane as it loses airflow. ?

(Although, in the case of the Ta152 and the Ki-84, the unrecoverable spins only happen due to a failed attempt to recover the plane's control in time when it has entered an elongated hammerhead)


 It's not the type of stall they are showing that should be questioned. Rather, what is to be questioned is;

"Are those common factors in the above mentioned planes, really so effective that it is enough to cause inverted flat spins so frequently than compared to other planes?"



[EDIT/ps] Pyro posted right before me, but I can see his answers might be source for another confusion.

 Pyro, by saying 'unintentional' what does it exactly mean? Does it mean;

a) The fact that only some of the mentioned planes entering "inverted flat spins" is unintentional

 or

b) The FM portraying the "inverted flat spin" itself, is unintentional

 ??
« Last Edit: February 08, 2007, 08:53:12 PM by Kweassa »

Offline hubsonfire

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HT, a Question about the Spit FM:
« Reply #37 on: February 08, 2007, 09:36:18 PM »
The original question was "is it something that should happen?", and the answer to that is "no, it's not intentional".

I would interpret this to mean that they didn't intend for the spit to do this.
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Offline Mace2004

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HT, a Question about the Spit FM:
« Reply #38 on: February 08, 2007, 11:17:15 PM »
Short explaination: (or Executive Summary)

Just to clarify a few things here guys.  All "spins" require yaw whether they be upright or inverted and the physics of upright and inverted are pretty much the same although the spins are not identical.  There are no if's and's or but's about this.  The bottom line is the inverted stall with no yaw described by Biggles isn't right, or as Pyro says, it's not intentional.



Spin 101:  "or, how to say the same thing but in a lot more words":

There are different things that can cause a spin but all spins need two components: stall and yaw.  If those two things don't exist there is no spin.  There's another situation that many will call a spin and that's when you're very nose low and rolling but this is a high speed spiral, not a spin and there is no stall and only low yaw rates.  The pilot keeps pulling on the stick but if he doesn't level his wings he just keeps tightening the spiral until he becomes one with terra firma.

Although the causes of a basic spin can be complicated it always starts out with a stall.  If you don't stall, you can't spin.  One wing stalls first (or is more stalled than the other wing) creating drag on that wing.  The drag yaws the airplane toward that wing and the unstalled (or less stalled) wing generates a bit of lift which cases the plane to roll into the stalled wing.  The roll increases the AOA of the stalled wing ensuring it stays stalled and keeps generating yaw due to drag while the roll decreases the AOA of the other wing ensuring the plane continues to roll so you have a self-perpetuating spin.  If the airplane isn't recovered the yaw rate continues to build and generates more and more centripetal force causing the nose to rise toward the horizon.  As the nose rises the yaw rate increases, roll decreases and the airplane enters a flat spin and you're in deep trouble in most airplanes.  

How quickly or even if a plane will enter a flat spin is based on the mass distribution and CG.  The more mass at the ends of the fuselage or wings the greater the tendancy to flat spin.  Think of a gyroscope where the weight is almost all located away from the center at the rim.  A flat spin works exactly the same way as a spinning gyroscope.  The most violent and deadly spin is the high-speed "coupled departure".  This occurs due to high rates in one axis generating high rates in another through gyroscopic precession, the two rates "couple" and you're off to the races.  In this an airplane can almost instantaneously generate severe yaw rates resulting in a departure going almost directly into a fully developed flat spin.  Airplanes have been known to come apart (engineers like to call this "structural divergence" while those with a more philosophical bent say "out of one, many".  Pilots usually say "oh, sXXt") in a high-speed coupled departure.

The physics of an inverted spin are identical.  You still have stall and yaw but the big difference is that the tail and rudder are now in the relative wind as opposed to being masked by the fuselage which means it's much easier to counter the yaw. Most inverted spins actually require the pilot to maintain pro-spin controls in order to maintain the spin otherwise most planes will recover on their own.

So much for Spin 101, back to AH.  Biggel's description is accurate but it happens in other airplanes as well including the Hurricane.  There is no yaw, hence, it is not a spin.  A better term is a low-speed "departure" which is short for "departure from controlled flight".  An even more specific description would be inverted pitch hangup or deep stall.  There may be more but the only airplane I know of that displays a similar tendancy is the F/A-18 Hornet but even if there are a few more it's an extremely rare departure mode.  Also, the Hornet does it upright, not inverted and it's related to a combination of it's flight control laws and the large leading edge extension (LEX) on both sides of the cockpit.  It also doesn't fall straight down, it'll oscillate as in a falling leaf maneuver.
« Last Edit: February 08, 2007, 11:23:55 PM by Mace2004 »
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Offline BaldEagl

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HT, a Question about the Spit FM:
« Reply #39 on: February 08, 2007, 11:29:01 PM »
Well it's definately a bug because it's happened to me in a Spit V with a wing blown off.  Upside down floating inverted to the ground at the speed of a chute.  You'd think missing a wing would make the plane roll over but nope.
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Offline Stoney74

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HT, a Question about the Spit FM:
« Reply #40 on: February 08, 2007, 11:31:43 PM »
I thought it was against the F-18 NATOPS to fly the Hornet cross-controlled?  :)

My only thought by posting the video was to counter the argument that the "relative wind" against the horizontal stab was enough to make the plane pitch forward.  I was able to duplicate the condition Biggles discussed in the Spit I, Hurri I, and Spit V, although when I turned the engine back on, the Spit V corrected itself on its own.  The P-47 would not do it, regardless of how uncoordinated I could get it.

Personally, I'm as curious to find out why it happens on these planes, and not others, given the overall precision of the stall model in the game, as shown by Skuzzy's post in WW's thread on the F4U and F6F.

Offline OOZ662

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HT, a Question about the Spit FM:
« Reply #41 on: February 08, 2007, 11:41:46 PM »
Quote
Originally posted by dtango
More than likely the aircraft transitioned from some form of flat spin to flat stall (where there is zero rotation around the yaw axis).  Spins occur because the left and right wings of the aircraft are producing different lift in a stall because the variation of angle of attack between the left and right wings for a variety of reasons.  As you near 90 angle of attack on both wings in a flat spin/stall it's conceivable that any spin is arrested by the natural directional (yaw) stability of the aircraft resulting in just a flat stall with little to no rotation around the directional (yaw) axis of the aircraft. [/B]


Nope. I'll film it when I have time. All I had to do was take a mossie vertical and force it to stay there until it slid like a leaf onto it's back and fell straight down and level inverted. I haven't done it in other aircraft because I never go straight up like that in fights and I don't fly any of the spits other than the 14.
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Offline Stoney74

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HT, a Question about the Spit FM:
« Reply #42 on: February 08, 2007, 11:46:48 PM »
WW's film demonstrates the problem, even though he doesn't get the planes inverted.  Its the same thing that gets 'em all kinked up going vertical.

Offline Major Biggles

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HT, a Question about the Spit FM:
« Reply #43 on: February 09, 2007, 04:22:17 AM »
cool, pyro, thankyou ;)

i don't know how easy it is to fix the flight model of a plane, is it something that can be fixed without too much hassle?

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Offline Badboy

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HT, a Question about the Spit FM:
« Reply #44 on: February 09, 2007, 06:35:00 AM »
Quote
Originally posted by Mace2004
An even more specific description would be inverted pitch hangup or deep stall.  There may be more but the only airplane I know of that displays a similar tendancy is the F/A-18 Hornet but even if there are a few more it's an extremely rare departure mode.  Also, the Hornet does it upright, not inverted and it's related to a combination of it's flight control laws and the large leading edge extension (LEX) on both sides of the cockpit.  It also doesn't fall straight down, it'll oscillate as in a falling leaf maneuver.


The F-16 has a deep stall that can be recovered by pitch rocking out of it. It can also occur inverted, and can be very smooth (non-oscillatory in pitch) and stable while in the deep stalled condition just like the Spitfire in this simulation. Or, depending on the configuration and entry conditions, the deep stall conditions can vary from smooth to highly oscillatory. Centerline stores tend to make the deep stall more oscillatory in pitch and depending on aircraft configuration, may cause the nose to slice left or right. I know of two F-16 simulations that model the deep stall and both only exhibit the smooth deep stalled condition similar to what we see in Aces High.

The type of deep stall that happens in Aces High can and does happen in real aircraft. Could it happen in the Spitfire? I'm not sure, but one of the cheapest ways to explore the question initially would be to build a simulation and see if it predicts that type of behaviour... HT already did, and it does. Is it right or wrong? I don't know off-hand, but it is interesting enough to investigate a little more. Perhaps HTC has discovered a previously unknown departure mode for the Spitfire?

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