Recorded airfoil sections

Panstwowe Zaklady Lotnicze PZL Mielec M-93 Iryda

The UIUC airfoil-usage tables record the Panstwowe Zaklady Lotnicze PZL Mielec M-93 Iryda with 2 airfoil sections. Each is in the library with its geometry, a stored polar sweep, and DXF and .dat export. The source lists names only — it does not say which station carries which section — so they appear here thickest first.

Sections side by side

SectionSeriesThicknessat x/cCamberat x/c
NACA 64A210NACA10.0%37%1.33%52%
NACA 64A-010 10.0%NACA10.0%37%symmetric—

NACA 64A210

NACA series · 10.0% thick at 37% chord · 1.33% camber at 52% chord

Also recorded on 5 other aircraft

NACA 64A-010 10.0%

NACA series · 10.0% thick at 37% chord · symmetric

Also recorded on 10 other aircraft

wing designs

The sections above are what the source records, not a wing anyone drew. Wings that were drawn — planform, sections and the analysis behind them, all readable — are published under Full-scale aircraft wing designs.

Aircraft-to-section mapping from the UIUC airfoil-usage tables. Section geometry is computed from the library's CST fit; nothing here is a performance claim about the aircraft. All recorded aircraft

Panstwowe Zaklady Lotnicze PZL Mielec M-93 Iryda airfoil: NACA 64A210 and NACA 64A-010 10.0% | Foil.tools