Analysis workflows
How to Detect Outliers and Unphysical Results in Airfoil Polar Data
HENDOI · 26 October 2026
A negative drag, a lift slope nothing like attached flow, or a point the solver did not converge is not a quirky airfoil. Flag it. Do not fair a curve through it.
Checks that do not require a better theory
The failed-polar lesson and the convergence lesson cover a solve that admits it failed. Outliers are the points that look like answers. Run these checks before a curve is published. They will not catch a subtle modeling error. They will catch the rows that should never enter a database.
| Symptom | What to do |
|---|---|
| CD below zero, or a drag far below skin friction at that Reynolds number | Drop the point. Profile drag of a real section is positive. |
| Attached-flow lift slope far from the thin-airfoil value of about 2π per radian, roughly 0.11 per degree | Inspect the case. A slope of half or double that, while the pressure plot is still attached, is usually a reference-area error, a radian-degree mix-up, or a bad geometry. The lift-slope lesson is the benchmark, not a law past stall. |
| CL or CM jumping between neighboring angles that both claim to be attached | Flag both. A real stall is a break you can see in CD as well. A single spike is often a solver hop. |
| A residual or a convergence flag that the method itself marks as failed | Omit the coefficients. The last iteration is not a polar point. |
| A moment that changes when you recompute it from the pressure plot at the stated reference | The stored CM and the stored pressures are not the same solution. Do not average them. |
Repeat a suspicious angle once. A point that moves by more than your tolerance is scatter or a bistable stall, and either way it does not get a smooth spline drawn through it. Record the rejection reason in the same table as the kept points. Silence looks like a clean curve and hides the hole.
Where this sits in the series
In simple words: what this page is for
A negative drag, a lift slope nothing like attached flow, or a point the solver did not converge is not a quirky airfoil. Flag it. Do not fair a curve through it.
This lesson exists because section decisions fail when geometry, method labels and selection reasons are scattered. How to Detect Outliers and Unphysical Results in Airfoil Polar Data helps you keep a clean trail from shape to polar to choice.
Why the topic matters
Engineers lose time when a title sounds clear but the page only sketches the idea. This article expands How to Detect Outliers and Unphysical Results in Airfoil Polar Data so you can answer three questions without jargon: what is the idea, when do you use it, and how do you check it in a HENDOI product.
Read the sections above for the core definitions. Use the steps below to move from reading into a real project trail you can share with a teammate.
How to apply this in HENDOI
In practice: create a HENDOI account or log in, open HENFOIL, bring a section in (create, import DAT, or digitize), pass the geometry gate, climb the analysis ladder only as far as the decision needs, then compare and archive. Every calculated number should keep its method label.
When the section choice is ready for the aircraft, continue in HENSYNTH for mission, compliance and trades. Same account. Same plans.
What this page will not claim: a teaching polar or geometry note is not a flight-Re certificate. HENFOIL labels methods so you know what you bought. Tunnel data and professional judgement still sit outside any single software run.
Checklist before you leave this page
- Can you state the idea of How to Detect Outliers and Unphysical Results in Airfoil Polar Data in one sentence?
- Do you know which product owns the next action — HENFOIL or HENSYNTH?
- Will every number you keep carry a method label or a stored-run source?
- If you are new here, have you opened Register or Login?
Related reading on this site
- Active Flow Control on Airfoils: Suction, Blowing and Synthetic Jets
- How Adverse Pressure Gradients Affect Airfoil Boundary Layer Separation
- What Is the Aerodynamic Center of an Airfoil? Location, Meaning and Applications
- What Is Airfoil Aerodynamic Efficiency Across a Range of Flight Conditions?
- All HENDOI blog articles
- HENFOIL product page
- HENSYNTH product page
- Pricing — Student, Professional & Team
- FAQ
- Login · Register now
- Previous: Airfoil sensitivity analysis
- Next: Airfoil solver benchmarking
- Index: all HENFOIL airfoil lessons
These pages teach the ideas. They are not wind-tunnel data and not a certification analysis. When a number matters, compute it at a stated Reynolds number, Mach number and transition setting, and keep the method label on the result. In HENFOIL that production polar is a VIC polar — see the analysis ladder and the polar field guide.
Both products live
Use this lesson in the HENDOI workspace
This page sits in Analysis workflows. HENFOIL and HENSYNTH are both live on one account. These articles are screening lessons — not certification reports.
Live · section
HENFOIL
Turn this lesson into a section you can draw, check, analyse and compare. Run the polar at the Reynolds number of the vehicle. The method name stays on the result.
To Know MoreLive · aircraft
HENSYNTH
After the section is chosen, set geometry and mission requirements, run screening, read compliance, synthesize candidates and download or mail the report.
To Know MoreAerospace industry collaboration
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