Avions Fairey (Tipsy) Junior airfoil?

cluttonfred

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Does anyone have a source identifying the airfoil used in the wing of the Tipsy Junior light plane by Avions Fairey in 1947?

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From the book "Les avions Tipsy / Tipsy airplanes" by Vincent Jacobs:

Tipsy S2: RAF 48 at the root, RAF 28 at the tip.
Tipsy Nipper: NACA 43012A
Gusty Nipper: NACA 0012
 

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  • Tipsy Junior Airfoil.JPG
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  • Tipsy S2 airfoil.JPG
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Thanks, I have that book, too, but I am still trying to identify the Junior airfoil in particular.
 
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Does anyone have the Putnam series Fairey Aircraft since 1915 handy? I wonder if the Tipsy types are covered in there given the Fairey connnection.
 
Fairey Aircraft covers 8 Tipsy types on pages 39-44.
 
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All it mentions about the Junior is that 2 were built. Airfoils are not mentioned for any of the aircraft in the book. What is so important about its airfoil?
 

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  • E. Clutton 11-2019 at FALL SMALL 2019.jpg
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I do know Eric, I have been running the site on his behalf for ten years!

On the Tipsy Junior, I am studying it from the point of view of an amateur builder, not to make a replica but to collect design tips and tricks, and the airfoil is a pretty fundamental data point.
 
IF you can get a decent (square on) photo of the aerofoil, it can be imported into XFLR5, traced and then analysed. This is an imperfect process but but in the absence of other data, it may be your best bet...?
 
IF you can get a decent (square on) photo of the aerofoil, it can be imported into XFLR5, traced and then analysed. This is an imperfect process but but in the absence of other data, it may be your best bet...?

I only have this image of a typical wing rib reproduced from a small image in the Jacobs book. I don't have the ability to pull the data from this image, but if you or someone else does and can thereby identify the airfoil, I'd be grateful.

tipsy junior rib detail.jpeg
 
I probably won't be able to ID the aerofoil but I should be able tell you what the characteristics are and if you tell me what the operating Re value is, generate a Cl vs Cd plot. I might take a 'short while' so *usual disclaimer applies' ;)
 
Thanks! Wing chord is about 5.0 ft and cruising speed about 98 mph in the Walter Mikron version so the Reynolds number is about 4.7 million.
 
Thanks, Mark, I know that site well.

Shed, I have to wonder if there might be some distortion in the image. I checked airfoiltools.com and I can't find any common 1940s or earlier airfoils very close to that camber and thickness. I did find the RAF 38 with 2.5% camber and 12.7% thickness which seems the most likely candidate.

 
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As promised plot attached.
tj1a is the aerofoil as traced and 1 and 2 are with a small amount of inverse design to clean the aerofoil up.

Not sure if it will upload but p2.wpa is the Xflr file. You're free to use this but obviously not for anything man-carrying, eh? ;) edit - can't upload .wpa files - sorry.
 

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Attached is the xflr file. I've named it p3.txt - download it and change the file extension to .wpa
 

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  • p3.txt
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