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Airfoil database list (S).

S9032 (9%) to NASA SC(2)-0406 AIRFOIL

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(s9032-il) S9032 (9%)

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S9032 (9%)Selig S9032 (9%) symmetrical horizontal stab airfoil used on the Blackhawk R/C sailplane
Max thickness 9% at 25% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9033-il) S9033 (7.5%)

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S9033 (7.5%)Selig S9033 (7.5%) symmetrical vertical stab airfoil used on the Blackhawk R/C sailplane
Max thickness 7.5% at 22.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9037-il) S9037 (9%)

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S9037 (9%)Selig S9037 (9%) low Reynolds number airfoil used on the Opus R/C sailplane
Max thickness 9% at 28.5% chord
Max camber 3.3% at 42.4% chord
Source UIUC Airfoil Coordinates Database

(sa7024-il) SA7024

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SA7024Selig / Ashok Gopalarathnam SA7024 low Reynolds number airfoil
Max thickness 7% at 25.9% chord
Max camber 3.3% at 43.3% chord
Source UIUC Airfoil Coordinates Database

(sa7025-il) SA7025

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SA7025Selig / Ashok Gopalarathnam SA7025 low Reynolds number airfoil
Max thickness 8% at 29.2% chord
Max camber 3.6% at 43.2% chord
Source UIUC Airfoil Coordinates Database

(sa7026-il) SA7026

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SA7026Selig / Ashok Gopalarathnam SA7026 low Reynolds number airfoil
Max thickness 9% at 32.9% chord
Max camber 3.8% at 47.1% chord
Source UIUC Airfoil Coordinates Database

(sa7035-il) SA7035

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SA7035Selig / Ashok Gopalarathnam SA7035
Max thickness 9.2% at 27.9% chord
Max camber 2.4% at 41.9% chord
Source UIUC Airfoil Coordinates Database

(sa7036-il) SA7036

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SA7036Selig / Ashok Gopalarathnam SA7036
Max thickness 9.2% at 28.1% chord
Max camber 2.6% at 42.1% chord
Source UIUC Airfoil Coordinates Database

(sa7038-il) SA7038

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SA7038Selig / Ashok Gopalarathnam SA7038
Max thickness 9.2% at 28.5% chord
Max camber 3% at 42.5% chord
Source UIUC Airfoil Coordinates Database

(saratov-il) SARATOV AIRFOIL

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SARATOV AIRFOILSaratov R/C sailplane airfoil
Max thickness 9.2% at 15% chord
Max camber 9.8% at 40% chord
Source UIUC Airfoil Coordinates Database

(sc1012r8-il) SIKORSKY SC1012R8 AIRFOIL

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SIKORSKY SC1012R8 AIRFOILSikorsky SC1012 R8 rotorcraft airfoil
Max thickness 12% at 27.8% chord
Max camber 2.7% at 21.8% chord
Source UIUC Airfoil Coordinates Database

(sc1094r8-il) SIKORSKY SC1094 R8 AIRFOIL

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SIKORSKY SC1094 R8 AIRFOILSikorsky/Velkoff SC1094 R8 rotorcraft airfoil
Max thickness 9.4% at 27.8% chord
Max camber 2.1% at 21.7% chord
Source UIUC Airfoil Coordinates Database

(sc1095-il) SIKORSKY SC1095 AIRFOIL

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SIKORSKY SC1095 AIRFOILSikorsky/Balch SC1095 rotorcraft airfoil
Max thickness 9.5% at 26.9% chord
Max camber 0.8% at 26.9% chord
Source UIUC Airfoil Coordinates Database

(sc1095r8-il) SIKORSKY SC1094R8 AIRFOIL

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SIKORSKY SC1094R8 AIRFOILSikorsky/Velkoff SC1095 R8 rotorcraft airfoil
Max thickness 9.3% at 26.5% chord
Max camber 2.1% at 20.5% chord
Source UIUC Airfoil Coordinates Database

(sc20010-il) NASA SC(2)-0010 AIRFOIL

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NASA SC(2)-0010 AIRFOILNASA SC(2)-0010 airfoil (NASA TP-2969)
Max thickness 10% at 37% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(sc20012-il) NASA SC(2)-0012 AIRFOIL

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NASA SC(2)-0012 AIRFOILNASA SC(2)-0012 airfoil (NASA TP-2969)
Max thickness 12% at 37% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(sc20402-il) NASA SC(2)-0402 AIRFOIL

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NASA SC(2)-0402 AIRFOILNASA SC(2)-0402 airfoil (NASA TP-2969)
Max thickness 2% at 34% chord
Max camber 0.5% at 83% chord
Source UIUC Airfoil Coordinates Database

(sc20403-il) NASA SC(2)-0403 AIRFOIL

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NASA SC(2)-0403 AIRFOILNASA SC(2)-0403 airfoil (NASA TP-2969)
Max thickness 3% at 36% chord
Max camber 0.6% at 85% chord
Source UIUC Airfoil Coordinates Database

(sc20404-il) NASA SC(2)-0404 AIRFOIL

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NASA SC(2)-0404 AIRFOILNASA SC(2)-0404 airfoil (NASA TP-2969)
Max thickness 4% at 37% chord
Max camber 0.7% at 81% chord
Source UIUC Airfoil Coordinates Database

(sc20406-il) NASA SC(2)-0406 AIRFOIL

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NASA SC(2)-0406 AIRFOILNASA SC(2)-0406 airfoil (NASA TP-2969)
Max thickness 6% at 35% chord
Max camber 0.6% at 79% chord
Source UIUC Airfoil Coordinates Database
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