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Propeller Design

Aviation Discuss Propeller Design in the World War II - Aviation forums; First off, great forum people. Now the question. I have always wondered as the war progressed why american planes went ...


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Old 07-19-2006, 08:25 PM   #1
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Propeller Design

First off, great forum people. Now the question. I have always wondered as the war progressed why american planes went to a broad four blade design of prop while the RAF seemed to favor a slender five blade design and the germans kept a large three blade paddle type. What were the reasons or benefits of each.
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Old 07-19-2006, 09:10 PM   #2
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It was all a matter of the methodology used by the engineers for squeezing the maximum amount of power from the engine while achieving maximum efficiency.
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Old 07-20-2006, 04:31 AM   #3
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It depends how fast you want your prop to spin. More blades are more efficient for a faster-spinning prop.
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Old 07-20-2006, 05:25 AM   #4
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I think it also had to do with the design of the aircraft and how to get the most from that aircraft. Some Luftwaffe aircraft had 4 blades instead of 3. Some British had 3 blades instead of 4. Some US aircraft had 3 instead of 4.
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Old 07-20-2006, 05:44 AM   #5
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I always thought that the general rule was the more hp the engine gives the more propeller blades it had
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Old 07-20-2006, 05:56 AM   #6
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I dont think so. Look at the Ta-152. It had well over 2000hp and only had 3 blades. Look at the Bf-109K and so forth.
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Old 07-20-2006, 09:43 AM   #7
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It even got as banal as the height of the landing gear struts positioning the nose above the runway for tail draggers at least. A shorter height gear kept the nose lower but limited the diameter of the blade arc. It is much easier to steer and see on the ground and easier to take off if the nose isn't pointed heavenward at a steep angle. So 4 blades of less over all diameter gave as much or more power than a large diameter 3 blade. A fighter had to still have clearance when you brought the tail up on takeoff when the fuselage was level.
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Old 07-20-2006, 11:22 AM   #8
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right, gotcha
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Old 07-20-2006, 12:01 PM   #9
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The P-47 was the first fighter to feature telescoping landing gear struts to give the gear more length when extended for this very reason.
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Old 07-20-2006, 01:20 PM   #10
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Quote:
Originally Posted by mosquitoman
I always thought that the general rule was the more hp the engine gives the more propeller blades it had
As I said before;

"It depends how fast you want your prop to spin. More blades are more efficient for a faster-spinning prop."

Which is why more modern wind turbines (well depending on where) have one propellor and a counterweight.
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Old 07-20-2006, 08:05 PM   #11
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Thank you gentlemen for your thoughts. I agree that height is an issue I beleve that is why the Vought F4U had a cranked wing. RPM's and horsepower may figure but as stated most late models had big HP numbers, although I'm not sure about RPM's. Maybe the materials used had an affect, (were German props made out of wood?). Tip speeds need to remain sub-sonic too. Anyway thanks again for answering this trivial question.
Oh, the best fighter of WW2?- F6F Hellcat!
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Old 07-20-2006, 08:06 PM   #12
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Propeller Design

Thank you gentlemen for your thoughts. I agree that height is an issue I beleve that is why the Vought F4U had a cranked wing. RPM's and horsepower may figure but as stated most late models had big HP numbers, although I'm not sure about RPM's. Maybe the materials used had an affect, (were German props made out of wood?). Tip speeds need to remain sub-sonic too. Anyway thanks again for answering this trivial question.
Oh, the best fighter of WW2?- F6F Hellcat!
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