A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Piloting
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

P-63 (?) Airacobra/Kingcobra power question



 
 
Thread Tools Display Modes
  #1  
Old November 3rd 09, 04:21 PM posted to rec.aviation.piloting
a[_3_]
external usenet poster
 
Posts: 562
Default P-63 (?) Airacobra/Kingcobra power question

On Nov 3, 10:55*am, Ron Wanttaja wrote:
a wrote:
My aerodynamic question had always been why there are fewer pusher
props. In a puller some of the wind energy is used up against the
airplane.


In a pusher, the prop has to operate in turbulent air stirred up by the
structure in front. *Depending on the design of the airplane, the prop
also has to be stronger (e.g., heavier) to withstand the cycling loads
if there's a wing or something blocking part of the prop disk from the
slipstream (think Long-EZ).

Ron Wanttaja


Thanks! I seem to remember the pusher in the C310 was less effective
too.
  #2  
Old November 3rd 09, 05:23 PM posted to rec.aviation.piloting
Steve Hix[_2_]
external usenet poster
 
Posts: 50
Default P-63 (?) Airacobra/Kingcobra power question

In article
,
a wrote:

On Nov 3, 10:55*am, Ron Wanttaja wrote:
a wrote:
My aerodynamic question had always been why there are fewer pusher
props. In a puller some of the wind energy is used up against the
airplane.


In a pusher, the prop has to operate in turbulent air stirred up by the
structure in front. *Depending on the design of the airplane, the prop
also has to be stronger (e.g., heavier) to withstand the cycling loads
if there's a wing or something blocking part of the prop disk from the
slipstream (think Long-EZ).

Ron Wanttaja


Thanks! I seem to remember the pusher in the C310 was less effective
too.


Cessna?

The C-336/337 turns out to perform slightly better in single-engine
flight on the rear engine than the front.
  #3  
Old November 4th 09, 03:22 AM posted to rec.aviation.piloting
Ron Wanttaja[_2_]
external usenet poster
 
Posts: 108
Default P-63 (?) Airacobra/Kingcobra power question

a wrote:
On Nov 3, 10:55 am, Ron Wanttaja wrote:
a wrote:
My aerodynamic question had always been why there are fewer pusher
props. In a puller some of the wind energy is used up against the
airplane.

In a pusher, the prop has to operate in turbulent air stirred up by the
structure in front. Depending on the design of the airplane, the prop
also has to be stronger (e.g., heavier) to withstand the cycling loads
if there's a wing or something blocking part of the prop disk from the
slipstream (think Long-EZ).

Ron Wanttaja


Thanks! I seem to remember the pusher in the C310 was less effective
too.


As Steve pointed out, you were thinking of the C336/337 Skymaster. It
*did* have a better rate of climb on the rear engine. One theory I read
was that it was due to the aerodynamics of the rather blunt back end
being better when there was an engine to help suck the air past....

There's no real pat answer; you can find efficient pusher aircraft, just
like you can find efficient tractor planes.

For an example, see:

http://www.ar-5.com/

Years ago, when there was a controversy as to whether paddles or
propellers were most efficient for ships, the British came up with a
simple test: They built two identical ships, with identical engines,
one with paddles and one with a prop. They tied a rope between the
sterns, and had the captains go to full power to see which had more thrust.

Pity you can't do this with a couple of airplanes....

Ron Wanttaja
  #4  
Old November 4th 09, 03:56 AM posted to rec.aviation.piloting
Jim Logajan
external usenet poster
 
Posts: 1,958
Default P-63 (?) Airacobra/Kingcobra power question

Ron Wanttaja wrote:
Years ago, when there was a controversy as to whether paddles or
propellers were most efficient for ships, the British came up with a
simple test: They built two identical ships, with identical engines,
one with paddles and one with a prop. They tied a rope between the
sterns, and had the captains go to full power to see which had more
thrust.


Wikipedia says that "In 1848 the British Admiralty held a tug of war
contest between a propeller driven ship, Rattler, and a paddle wheel ship,
Alecto. Rattler won, towing Alecto astern at 2.5 knots (4.6 km/h)...."

http://en.wikipedia.org/wiki/Propeller

However, it is probable that the paddle wheel ship simply didn't have the
right size paddles. Paddle wheels should be capable of efficiencies similar
to propellers - but it takes very large wheels.
  #5  
Old November 4th 09, 06:19 AM posted to rec.aviation.piloting
Ron Wanttaja[_2_]
external usenet poster
 
Posts: 108
Default P-63 (?) Airacobra/Kingcobra power question

Jim Logajan wrote:

However, it is probable that the paddle wheel ship simply didn't have the
right size paddles. Paddle wheels should be capable of efficiencies similar
to propellers - but it takes very large wheels.


Jim, Jim, Jim.... HOW can you set us up with a straight line like that?

1. "It's not the size of the wheels, it's how you use them."

2. "If they would have set up the wheels in a canard configuration, it
would have been more efficient."

:-)

Ron Wanttaja


  #6  
Old November 4th 09, 11:55 AM posted to rec.aviation.piloting
a[_3_]
external usenet poster
 
Posts: 562
Default P-63 (?) Airacobra/Kingcobra power question

On Nov 4, 1:19*am, Ron Wanttaja wrote:
Jim Logajan wrote:
However, it is probable that the paddle wheel ship simply didn't have the
right size paddles. Paddle wheels should be capable of efficiencies similar
to propellers - but it takes very large wheels.


Jim, Jim, Jim.... HOW can you set us up with a straight line like that?

1. *"It's not the size of the wheels, it's how you use them."

2. *"If they would have set up the wheels in a canard configuration, it
would have been more efficient."

:-)

Ron Wanttaja


Paddle wheels got screwed. It's just another demonstration that the
spinning thing belongs on the back of the hull.
  #7  
Old November 4th 09, 12:06 PM posted to rec.aviation.piloting
Steven P. McNicoll[_2_]
external usenet poster
 
Posts: 721
Default P-63 (?) Airacobra/Kingcobra power question

a wrote:

Paddle wheels got screwed. It's just another demonstration that the
spinning thing belongs on the back of the hull.


Except when it belongs in the front.

"At full load the Mackinaw displaced 5,252.4 tons and drew 19' 2.25" of
water. Her innovative features included a 12 foot diameter bow propeller
which draws water from beneath the ice ahead, both weakening the ice and
sending water along the sides of the hull and reducing ice friction. The
Mackinaw also has a heeling system which can shift nearly 112,000 gallons of
ballast water from side to side in 90 seconds, allowing a rocking motion
which assists the Mackinaw in freeing itself from ice."

http://www.mightymac.org/cgcmackinaw.htm


 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
US 269021 P63 Kingcobra 20070927 Columbus OH Graham Harrison[_2_] Aviation Photos 0 August 14th 08 06:27 PM
Engine power question??? [email protected] Home Built 24 October 13th 07 02:40 AM
Ship's Power (or portable GPS) Question Kyle Boatright Home Built 9 May 29th 07 03:17 PM
O-360 takeoff power fuel flow question argon39 Owning 13 August 2nd 05 05:23 PM


All times are GMT +1. The time now is 04:05 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.