Angle of incidence
Angle of incidence
Can anyone tell me the true Angle of Incidence of the inboard rib on the champ and chief.
- Nathan K. Hammond
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flyingfool
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Paul Agaliotis
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- Scott Rower
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If the tail on the Champ is the same on the Chief, it does.
do you have one of those for the chief, or know where I can look?
I'll try www.aeronca.com when I get to a computer faster than this dialup I'm on at the moment
Thanks
do you have one of those for the chief, or know where I can look?
I'll try www.aeronca.com when I get to a computer faster than this dialup I'm on at the moment
Thanks
- David Johnson
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The tail surfaces are the same as Joe says. However, the tail incidence is different. It is in each manual. I am at Sun n Fun and cannot look it up. The Chief has less incidence. I have always believed it is the reason for the speed difference. Chief has less CG change to deal with with different loading. David J.
Using drawing 4-901A horiz stab and drawing 7-580 fuselage, I come up with the following dimensions and angle
Centerline of tubes front to rear Horz stab 22.5"
Heighth of front tube C/L above reference line 16 1/4"
Heigth of rear tube C/L above reference line 18 3/32"
difference in heighth over 22.5 " is 1.84375 = -4.7 deg
this should be the horiz stab angle of incidence unless some of my dimensions are wrong.
However, two diferent 11 series operating online manuals list the figure as -3.5 deg
Centerline of tubes front to rear Horz stab 22.5"
Heighth of front tube C/L above reference line 16 1/4"
Heigth of rear tube C/L above reference line 18 3/32"
difference in heighth over 22.5 " is 1.84375 = -4.7 deg
this should be the horiz stab angle of incidence unless some of my dimensions are wrong.
However, two diferent 11 series operating online manuals list the figure as -3.5 deg
Scott Rower wrote:Hope this helps.
Also, the chord line on a 4412 airfoil is not the bottom of the airfoil.
Scott
I find it very interesting that this particular drawing lists the angle of incidence on the horiz stab at -3.5* when the service manual lists the angle of incidence for the tail surface at 5* for the 7AC and 3.5 for the 11AC.
I've posted ssome measurements from my 11CC on the next entry.
