747-300 from KLM had “strip” indicators for engine parameters.
Because of high failure rate they fell out of favour……………
See this list from : http://www.enginehistory.org
Look at the Engine model , as soon as there is an S in the model the “normal” horsepower is given at a certain altitude.
For example :
D-1 –> 550 Hp at 2100 RPM at S.L ( Sea Level )
SD-1 –> 500 Hp at 2000 RPM at 7500 Feet
And you are right at a certain speed the Mixer will become a Blower
The difference between Charged and Supercharged is that the compressor on a Supercharged engine can deliver more air on the ground then the engine can handle power wise ( so it can be overcharged – to high manifold pressure ). As such a super charged engine can deliver maximum horsepower up to a certain altitude because it can still deliver enough compressed air to reach maximum horsepower. A Charged engine reaches maximum power on sealevel and this power only decreases with altitude.
To : Mondariz
What did you do wrong to be a :
Rank 5 Registered User
with 1344 posts ???????????
๐
Interesting to see with these finds is that the use of “engine with crate” often leads to the misconception that it is a new engine. This probably caused by the car restauration scene where the phrase “crate engine” stands for a whole new engine.
If an aircraft is indeed a new and/or freshly overhauled example the engine logbooks would be present in the crate.
Stuart Gowans said :
if I were designing something that had two options, one of which was asthetically more pleasing, I know which one I’d go for, irrespective of cost or manufacturing issues.
I then wonder what you are thinking of when your design is up there defending your country and you are almost losing the battle ( of Britain ).
“Well I could have produced more planes if I kept my design simple and won the battle, but what the heck if you go down, go down in style !” ๐
Cheers Pim
PS : Stuart to lower your language barrier towards English , I can recommend to spend a long vacation in Britian or to watch a lot of BBC. Myself , I had the luck to work in Canada for 3 years. :p
To Stuart Gowans,
I think you made a small error. ๐
First you use a thorough investigation as proof that they knew what there were doing at Supermarine and then it seams that this investigation was done after the last Spitfire left the building. I have never met a designer who started to make calculations when the product is already flying around. So if this investigation was made by Supermarine afterwards they must already have know that the elliptical wing was probably a poor choice.
Then you use this investigation that concludes that there wasn’t a significant differance between the elliptical Spitfire wing or a trapered wing to proof again that they knew what they were doing.
So if the design department of Supermarine knew what they were doing then they knew that aerodynamics gains would minimal ( your qoute doesn’t say by the way which design is 1% better ) why in the hell would you go for elliptical wing platform which is very difficult to produce ?
My conclusion : If they knew what they were doing there can only be 2 reasons for an elliptical wing – space requirements or estetics
Then a small afterthought. An elliptical wing I can understand but an all elliptical tail section must have been pure estetics and has nothing to do with common sense
Cheers, Pim ๐
Thanks Stuart Gowens,
for your quote :
Quoting from the one book that will surely feature on Joglo’s christmas list; Spitfire the history, “an aerodynamicist has calculated that to arrive at an accurate total weight, each rib, spar, etc, must have been investigated and the whole assessed for aerodynamic performance; after all this effort by the drawing office, it was estimated that the aerodynamic performance difference between the straight taper and elliptical wing, was less than 1% at high speeds“
Then see the post of Webpilot quote :
Alfred Price’s ‘Spitfire – A Documentary History’, quotes Shenstone as saying:
” It has been suggested that we at Supermarine had cribbed the wing shape from that of the He70 transport. This was not so. The elliptical wing had been used on other aircraft and its advantages were well known. Our wing was much thinner than that of the Heinkel and had a quite different section. In any case it would have been simply asking for trouble to have copied a wing shape from an aircraft designed for an entirely different purpose”.
These 2 references contradict eachother. :confused:
If they did a complete survey into the differences between the 2 wing platforms and didn’t found a significant differance in performance then clearly the layout of the wing was done because of the need for space inside of the wing.
Ofcourse having a elliptical wing in those days could have been a aerodynamic sales pitch
Greetings Pim
Clearly the design staff at Supermarine didnโt understand the basic idea behind the elliptical shaped wing . The Aerodynamic goal is to achieve an elliptical lift profile, this is quit different than an elliptical wing. The easiest way to achieve this is to use an elliptical wing platform and to use only 1 airfoil for the whole wing with a constant incidence.
For a better explanation see : http://courses.ae.uiuc.edu/AE440-A/files/Aerodynamics_Overview.pdf
If you then use 2 different airfoils ( spitfire naca2213 โ naca2208 ) and you apply washout then you kill the whole idea behind it. ๐ฎ
The designers at Republic knew the basic idea , because they used for the P47 an elliptical wing, 1 airfoil and no washout.
With a trapezium shaped wing it is possible to come close to an elliptical lift profile by carefully choosing the taper , the inboard and outboard airfoil and washout or washin.
To the defense of the Supermarine design staff , I must say that probably the elliptical lift profile was classified German information. They saw an elliptical wing with good characteristics and thought probably that the shape was the secret of success. If they knew the aerodynamic principle behind it then clearly the shape of the Spitfire was a result of putting all the stuff in a minimum thickness wing.
I ( as an design engineer myself ) think the truth is somewhere in the middle. As an engineer you constantly look to the competition for inspiration, but afterwards you cannot speak of an eureka moment in your own design.
Cheers Pim
Dear Proctor VH-AHY,
Please don’t stop reading after the first sentence , you forgot to mention that Wikipedia also says :
– the pure elliptical shape as an ideal planform may be a myth
– furthermore, the wing’s uniform lift distribution causes the entire span of the wing to stall simultaneously, potentially causing loss of control with little warning. To compensate, aircraft such as the Supermarine Spitfire used a modified elliptical wing with washout, though such compromises increase induced drag and reduce a wingโs efficiency
It would be interesting to find some windtunnel research done in the 1930’s which confirms the overall better performance of elliptical wings over trapezium wing platforms.
Greetings, Pim
I agree with you Mondariz,
To put it in myth busters words :
Plausible, highly unlikely but still plausible,
greetings,
Pim Pouw
Fokker G1 replica
http://www.fokker-g1.nl
Strike three ………………..out ๐
Searcy Field, Stillwater, Oklahoma
Mondariz , any guess were it is located in the USA ?
Try this, in the smack middle……………1000 Naut.Miles from the East and West coast. Flying directly from a pacific base ????
A good guess is better than a false assumption……………..
Let’s take a B17 bomber, it cruises at aprox. 160 Knots. Within 250 Naut.Miles you have both states Oklahoma and Kansas covered. That is in flying time : 1 hour 35 minutes.
Then go to :
http://en.wikipedia.org/wiki/Oklahoma_World_War_II_Army_Airfields
http://en.wikipedia.org/wiki/Kansas_World_War_II_Army_Airfields
You will find 23 military airbases in WWII ๐
Then look at the list of aircraft Paul Mantz bought. A lot of aircraft start with a T, that is T from Trainer. Then ask yourself what were all those airfields for in the smack middle , perhaps Training ? ๐
All this together also explaines the very low price which was paid for the aircraft. Whoever wants to buy abused trainer aircraft in the middle of the USA ?
Pim Pouw
Fokker G1 replica
http://www.fokker-g1.nl
Oke let’s have a realistic look at the Paul Mantz’s purchase of 475 aircraft.
475 aircraft consisting of 134 fighters, 36 medium bombers, 305 heavy bombers.
These aircraft were flown to a civil airfield “Searcy Field”. Normally when you do a cross country flight you take a half an hour of extra fuel for safety matters. Now think positive and suppose the average fuel left in these aircraft was for 45 minutes.
134 Fighters X 45 min X 65 Gallon per hour = 6532 Gallon
36 M.Bombers X 45 min X 100 Gallon per Hour = 2700 Gallon
305 H.Bombers X 45 min X 200 Gallon per hour = 45750 Gallon
Total fuel = aprox 55000 Gallon = $ 16500 ๐
But still not even close to $55425.68 ๐ก
Like before I have heard this myths in connection with a lot of scrap aircraft.
I think Paul Mantz came the closest of fulfilling this myth.
Would be nice what was paid for a scrap B52, anyone ??
The car fuel price source see : http://www1.eere.energy.gov/vehiclesandfuels/facts/2005/fcvt_fotw364.html
Pim Pouw
Fokker G1 replica project
http://www.fokker-g1.nl
To me it looks like an “compression ignition engine”. Most people would call this a diesel. This early type of diesel would have run on a more eplosive mixture like petrol mixed with ether.
Why ?
-The valves setup makes it a combustion engine
– Lack of source of ignition
– the screws on the top of the domes are probably connected to a moving top cilinder which were used to regulate the compression ratio of the engine ( very important on a “diesel” ), this setup is still used on modelplane diesel engines
– early “diesels” had the nasty habit of exploding sometimes , so I think the studs together with the opening above the inlet valves were used for a safety valve sytem
Pim Pouw
Early Birds Foundation
the Netherlands
Where are they now? Maybe one in the Netherlands…
Hi Ritch & Max,
I am the owner of a Bede 5 kit ( B wings ) in the Netherlands.
I am certainly not the first owner , for sure is that I am at least
the third owner. I bought my kit in Belgium, partly built and ofcourse not complete.
I believe ( but are not certain ) that the kit came from the UK. From the original papers I have from the kit the first owners name emerged as :
Deane B. Fenton with a postal adress of ESSO refinery in Antwerp Belgium.
This name sounds very Britisch and certainly not from Belgium ! further to use your company name as postal adress sounds to me like someone working abroad.
Also for me it would be nice to know a little bit more of the origin of my BD5.
Greetings,
Pim
the Netherlands