The problem to be solved is that of turbulent flows around a Clark-Y airfoil. The camber and thickness are calculated in the Y direction.
This example uses Solidworks 2015, but it should work with any recent version of the software. The UIUC Airfoil Data Site gives some background on the database. I have had a few people ask me about the design and build of this wing.
I need this airfoil for my French 1/2A "Piaf" model designed by Patrick Nicolas. The airfoils are listed alphabetically by the airfoil filename (which is usually close to the airfoil name). I am looking for a flat bottomed airfoil near 12% thickness with the advantages of newer design, any suggestions? Simple and fast tip for creating a NACA airfoil using coordinates. After leaving Piper, Taylor designed the Taylorcraft.
I have no real knowledge about airfoils but after a bit of researching on the net, I decided upon either the Clark-Y … I thought I would share the way I designed a completely flat bottom Clark Y type airfoil. ANSYS Fluent: NACA 2412 airfoil with Angle of Attack Rotation and Varying Inlet velocity - Duration: 20:28. The dat file data can either be loaded from the airfoil database or your own airfoils which can be entered here and they will appear in the list of airfoils in the form below. Clark Y is the name of an airfoil that is widely used in aircraft design. Reynolds number is 143,000 based on the inlet velocity and airfoil chord length. There is the option to plot the camber around the circumference of a circle and adjust the plotting grid. Well, I found coordinates for a Clark Y airfoil while at work, and went ahead and plotted it manually (well, not entirely manually, let's just say thank god for copy/paste functions!). The following figures show the illustrations for C type and O type domains (Note: the figures are not in the exact scale as the true size of the domain and airfoil).
If it is the later, when the flat bottom portion of the wing is parallel with the center line of the fuse the wing will be at 2-3 degrees incidence. If anyone would like it emailed to them, just PM me.
As you can see on this drawing from 1979 published in the French "Modèle Magazine" , the shape of the airfoil is approximate. I have used the Clark Y airfoil for all my model airplane designs, from …
SUBSONIC WIND-TUNNEL WALL CORRECTIONS ON A WING WITH A CLARK Y-14 AIRFOIL A Masters Project Presented to The Faculty of the Department of Mechanical and Aerospace Engineering San Jose State University In Partial Fulfillment Of the Requirements for a Degree Master of Science In Aerospace Engineering By Tommy James Blackwell May 2011 Included below are coordinates for nearly 1,600 airfoils (Version 2.0). The dat file is in Selig format. So on the Clark Y, is the flat bottom of the wing the incidence line or do you draw a line from the most forward part of the airfoil to the most rear ward point of the trailing edge. Add your own airfoils so they can be used in the tools. You can insert this and crop it into a MSWord doc and size it by click on the picture and then pulling a corner to where the size is as big or as small as you need. Max camber 3.4% at 42% chord Source UIUC Airfoil Coordinates Database Source dat file The Clark Y is an airfoil widely used in aircraft wing design. So i am going to make some videos on how i went about making this wing.
The UIUC Airfoil Data Site gives some background on the database.
I hate approximations.
(Note: the figures are not in the exact scale as the true size of the domain and airfoil).
An additional feature of this airfoil is that its lower surface is parallel to its chord and this enables the use of an inclinometer to change the angle of attack directly. CLARK Y airfoil (smoothed) Max thickness 11.7% at 30.9% chord. The airfoils are listed alphabetically by the airfoil filename (which is usually close to the airfoil name).
Mohammed Khateeb 22,197 views Howdy folks: The Clark Y airfoil has a camber of 3.6% and a thickness of 12% depending on whose data you’re looking at. I need this airfoil for my French 1/2A "Piaf" model designed by Patrick Nicolas. EDIT: It was Link Click Here Here's a few airfoils from the book Flying Scale Models by R. G. Moulton. The airfoil chosen for this experiment was the Clark Y, a general purpose airfoil used for its superb control at low Reynolds numbers. Calculating the camber and thickness.
Included below are coordinates for nearly 1,600 airfoils (Version 2.0). I am by …
Source UIUC Airfoil Coordinates Database.
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