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Profile Generator (Airfoil) CustomFeature airfoil database has error for some common airfoil shapes.
john_longphre
Member Posts: 13 PRO
Hi. This tool is super old but super useful for me.
The NACA 23015 and NACA 23018 are two of the most widely used airfoil sections on aircraft (from the Beechcraft Bonanza to the Focke-wulf 190 and tons of other aircraft).
The ProfileGenerator Custom feature is great but it has a few errors in the source data for these two airfoils. Long lines are produced instead of proper airfoil shapes.
The owner/creator of this feature has abandoned the feature. No response after multiple attempts to contact him.
How can we edit the airfoil coordinates database? (I am new to FeatureScript and am bewildered, frankly).
In ProfileGenerator's Featurescript editor, I see this:
"aerofoil" : lookupTablePath({ "Aerofoil" : "NACA 23015", "DataBase" : "UIUC" })
I think the custom feature's UIUC database must have an error for these two airfoils:
From UIUC Airfoil Data Site (illinois.edu) ,the correct coordinates for NACA 23015 are:
The correct coordinates for NACA 23018 are:
The NACA 23015 and NACA 23018 are two of the most widely used airfoil sections on aircraft (from the Beechcraft Bonanza to the Focke-wulf 190 and tons of other aircraft).
The ProfileGenerator Custom feature is great but it has a few errors in the source data for these two airfoils. Long lines are produced instead of proper airfoil shapes.
The owner/creator of this feature has abandoned the feature. No response after multiple attempts to contact him.
How can we edit the airfoil coordinates database? (I am new to FeatureScript and am bewildered, frankly).
In ProfileGenerator's Featurescript editor, I see this:
"aerofoil" : lookupTablePath({ "Aerofoil" : "NACA 23015", "DataBase" : "UIUC" })
I think the custom feature's UIUC database must have an error for these two airfoils:
From UIUC Airfoil Data Site (illinois.edu) ,the correct coordinates for NACA 23015 are:
NACA 23015 1.0000 ...... 1.0000 (0.0016) 0.9500 0.0112 0.9000 0.0204 0.8000 0.0373 0.7000 0.0525 0.6000 0.0661 0.5000 0.0774 0.4000 0.0859 0.3000 0.0905 0.2500 0.0908 0.2000 0.0892 0.1500 0.0852 0.1000 0.0764 0.0750 0.0690 0.0500 0.0589 0.0250 0.0444 0.0125 0.0334 0.0000 ...... 0.0000 0.0000 0.0125 -0.0154 0.0250 -0.0225 0.0500 -0.0304 0.0750 -0.0361 0.1000 -0.0409 0.1500 -0.0484 0.2000 -0.0541 0.2500 -0.0578 0.3000 -0.0596 0.4000 -0.0592 0.5000 -0.0550 0.6000 -0.0481 0.7000 -0.0391 0.8000 -0.0283 0.9000 -0.0159 0.9500 -0.0090 1.0000 (-0.0016) 100.00 0.0000
The correct coordinates for NACA 23018 are:
NACA 23018 1.0000 0.0019 0.9500 0.0132 0.9000 0.0239 0.8000 0.0440 0.7000 0.0618 0.6000 0.0775 0.5000 0.0905 0.4000 0.1004 0.3000 0.1055 0.2500 0.1056 0.2000 0.1036 0.1500 0.0986 0.1000 0.0883 0.0750 0.0801 0.0500 0.0692 0.0250 0.0529 0.0125 0.0409 0.0000 0.0000 0.0125 -0.0183 0.0250 -0.0271 0.0500 -0.0380 0.0750 -0.0460 0.1000 -0.0522 0.1500 -0.0618 0.2000 -0.0686 0.2500 -0.0727 0.3000 -0.0747 0.4000 -0.0737 0.5000 -0.0681 0.6000 -0.0594 0.7000 -0.0482 0.8000 -0.0348 0.9000 -0.0194 0.9500 -0.0109 1.0000 -0.0019Is there some way to correct the database used by the ProfileGenerator custom feature?
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Comments
The other problem with the old custom feature, aside from being largely abandoned, is the use of opFitSpline [edited to correct: skFitSpline is what I meant - same issue though] to create the splines between all the raw data points. If you look at NACA23024 (which does successfully build) you'll see an... um... undesirable curvature plot. Zooming in you'll see issues at the leading edge (the two splines are not tangent) and so on.
Fortunately there is likely to be a new custom feature (completely unrelated to the old one) coming out very, very shortly! You'll want to check that out when it launches.
https://forum.onshape.com/discussion/24730/new-custom-feature-havf-profiles-standard-airfoil-profiles#latest