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FM/DM threads Everything about FM/DM in CoD

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  #1  
Old 12-20-2012, 03:21 AM
ATAG_Dutch ATAG_Dutch is offline
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Quote:
Originally Posted by Crumpp View Post
That is wrong.
Quote:
Originally Posted by ACE-OF-ACES View Post
Bingo!
Nothing changes here, does it?

Oil temp. Whatever settings people tell you to fly at, fly at less, apart from airspeed. Whether it be RPM or boost. Most people in a game fly at max poss everything all the time. Total rubbish.

What is the oil temp at which your engine blows? Find out. Run your mouse over the oil temp gauge and wait for it. Try it at different rpms. Try it at different boost settings. Just fly. Offline until you find out. Then you'll know.

Everything is there for you to find this out for yourself. Go to it.

Edit: 97 degrees. If memory serves correctly........

Last edited by ATAG_Dutch; 12-20-2012 at 01:21 PM.
  #2  
Old 12-21-2012, 11:47 PM
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Crumpp Crumpp is offline
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Quote:
Indicated airspeed is what matters, if indicated is high enough then cooling will be sufficient.


Why don't you take the time to explain the relationship of Indicated airspeed, True airspeed, and altitude?

Then take some to explain the general behavior of a altitude effects on thrust production at constant power setting and indicated airspeed.

After you have done that, you can sum it all up as:

Quote:
Crumpp says:

The higher you go, the less effective the cooling due to pressure and density reduction despite the cooler temperatures.
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  #3  
Old 12-22-2012, 08:06 AM
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Quote:
Originally Posted by Crumpp View Post


Why don't you take the time to explain the relationship of Indicated airspeed, True airspeed, and altitude?

Then take some to explain the general behavior of a altitude effects on thrust production at constant power setting and indicated airspeed.

After you have done that, you can sum it all up as:
OK then:

if you climb at constant airspeed then true airspeed increases with altitude, at constant indicated airspeed the 'mass' of air flowing through the cooling system remains constant with the added effect of reduced ambient temperatures.
penalties of high altitude on performance are not really a factor, bottom line is if you keep the same amount of air mollecules passing through the cooling system then you won't have problems cooling, I'm not entirely sure where crumpp gets the theory that maintaining constant indicated airspeeds is not possible but everyone else understands that a constant reading on the airspeed indicator means constant indicated airspeed and we also know how to achieve it.
To some extent engine temperatures will also fall off with the natural reduction of power with altitude also.


Oh and

Looking forward to the next installment from the Nonsensical Administration of Crumpp Aeronautics

p.s. I'll post you a picture of what high altitude shows on the Learjet PFD tonight as I have an empty sector back from Denmark tonight.
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Last edited by bongodriver; 12-22-2012 at 08:19 AM.
  #4  
Old 12-22-2012, 05:46 AM
JtD JtD is offline
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Quote:
Originally Posted by ATAG_Dutch View Post
Nothing changes here, does it?
Annoying, isn't it? I don't think this is the best subject to make generalisations, because temperature over altitude characteristics depend on aircraft, engine, engine settings, flying regime. So I suggest to find a different excuse for being rude to each other.
  #5  
Old 12-22-2012, 09:14 AM
NZtyphoon NZtyphoon is offline
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Originally Posted by JtD View Post
Annoying, isn't it? I don't think this is the best subject to make generalisations, because temperature over altitude characteristics depend on aircraft, engine, engine settings, flying regime. So I suggest to find a different excuse for being rude to each other.
I suggest that no-one argue with Crumpp because it is patently obvious that he is THE undisputed expert on everything.
  #6  
Old 12-22-2012, 09:54 AM
JtD JtD is offline
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It's not a Crumpp problem here. The generalizations are pointless.

Indicated air speed is not equivalent to mass flow, because there's a square root over density in the IAS calculation. At a constant IAS, mass flow goes down with altitude. WW2 aircraft generally achieved lower IAS's with altitude, so mass flow goes down even more. This is countered by the reduced temperatures at altitude.

Now you can argue all day about the net effect, but unless you come up with a statistically significant number of test results, it will remain pointless. What remains is an unnecessary exchange of rudeness, which I think this forum has seen enough.
  #7  
Old 12-22-2012, 07:25 PM
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JtD,

It is a basic principle of heat exchanger efficiency. It is not really open to much discussion and the fact so much is made of such a simple thing is telling.



Bongodriver, by all means post your findings. You might learn something.

Take a guess what the p is in the formula??

Don't let that stop you from posting the findings from a turbojet. We can then change the subject to some basic properties of thrust producers! Like I said, you will learn something!
Attached Images
File Type: jpg Heat Exchanger Efficiency.jpg (8.4 KB, 6 views)
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Last edited by Crumpp; 12-22-2012 at 07:29 PM.
  #8  
Old 12-22-2012, 07:50 PM
JtD JtD is offline
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Quote:
Originally Posted by Crumpp View Post
It is a basic principle of heat exchanger efficiency. It is not really open to much discussion and the fact so much is made of such a simple thing is telling.
The basic principle of heat exchangers seems to be clear to everyone, including bongodriver.

But:
- basic principles of heat exchangers don't fully explain general aircraft engine oil temperatures
- general aircraft engine oil temperature characteristics don't fully explain Spitfire specific oil temperatures
- detailed Spitfire oil temperature info won't change a thing in game, because development is dead
  #9  
Old 12-23-2012, 06:42 PM
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bongodriver bongodriver is offline
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Quote:
Originally Posted by Crumpp View Post
JtD,

It is a basic principle of heat exchanger efficiency. It is not really open to much discussion and the fact so much is made of such a simple thing is telling.



Bongodriver, by all means post your findings. You might learn something.

Take a guess what the p is in the formula??

Don't let that stop you from posting the findings from a turbojet. We can then change the subject to some basic properties of thrust producers! Like I said, you will learn something!
Learn something from you?......I doubt it.

I'm not posting pics for means of making revelations other than gratuitous 'look at me here at FL400 taking pics for my forum buddies', I couldn't post yesterday because I didn't make it back to home base before they closed and diverted to Luton, hotel had crappy wifi and I only had my phone, still it meant I got to take some more pics of todays sectors to Stuttgart and Sion, the latter being very Christmassy so I thought they'd go nice.

pics 1,2 on way back from Aalborg yesterday, pic 3,4 on ramp at Luton this morning, pic 5 on ramp at Stuttgart.
Attached Images
File Type: jpg 20121222_201214.jpg (1.58 MB, 29 views)
File Type: jpg 20121222_201342.jpg (1.39 MB, 25 views)
File Type: jpg 20121223_082203.jpg (2.28 MB, 29 views)
File Type: jpg 20121223_082303.jpg (1.93 MB, 21 views)
File Type: jpg 20121223_130244.jpg (2.13 MB, 18 views)
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  #10  
Old 12-23-2012, 06:50 PM
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Heres the Christmassy ones, the amazing view approaching the Swiss Alps and the descent on the 'IGS' approach to Sion.

Merry Christmas everyone, maybe we'll be nicer to each other next year....
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File Type: jpg 20121223_134807.jpg (1.64 MB, 16 views)
File Type: jpg 20121223_134816.jpg (1.36 MB, 12 views)
File Type: jpg 20121223_140745.jpg (2.22 MB, 17 views)
File Type: jpg 20121223_140756.jpg (3.32 MB, 19 views)
File Type: jpg 20121223_140812.jpg (2.05 MB, 17 views)
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