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Airfoil database list (H).

HQ 3.0/14 AIRFOIL to HT08

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(hq3014-il) HQ 3.0/14 AIRFOIL

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HQ 3.0/14 AIRFOILQuabeck HQ 3.0/14 R/C sailplane airfoil
Max thickness 14% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3015-il) HQ 3.0/15 AIRFOIL

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HQ 3.0/15 AIRFOILQuabeck HQ 3.0/15 R/C sailplane airfoil
Max thickness 15% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq308-il) HQ 3.0/8 AIRFOIL

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HQ 3.0/8 AIRFOILQuabeck HQ 3.0/8 R/C sailplane airfoil
Max thickness 8% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq309-il) HQ 3.0/9 AIRFOIL

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HQ 3.0/9 AIRFOILQuabeck HQ 3.0/9 R/C sailplane airfoil
Max thickness 9% at 35% chord
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3510-il) HQ 3.5/10 AIRFOIL

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HQ 3.5/10 AIRFOILQuabeck HQ 3.5/10 R/C sailplane airfoil
Max thickness 10% at 35% chord
Max camber 3.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3512-il) HQ 3.5/12 AIRFOIL

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HQ 3.5/12 AIRFOILQuabeck HQ 3.5/12 R/C sailplane airfoil
Max thickness 12% at 35% chord
Max camber 3.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3513-il) HQ 3.5/13 AIRFOIL

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HQ 3.5/13 AIRFOILQuabeck HQ 3.5/13 R/C sailplane airfoil
Max thickness 13% at 35% chord
Max camber 3.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3514-il) HQ 3.5/14 AIRFOIL

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HQ 3.5/14 AIRFOILQuabeck HQ 3.5/14 R/C sailplane airfoil
Max thickness 14% at 35% chord
Max camber 3.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq3518-il) HQ 3.5/18 AIRFOIL

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HQ 3.5/18 AIRFOILQuabeck HQ 3.5/18 R/C sailplane airfoil
Max thickness 18% at 35% chord
Max camber 3.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq358-il) HQ 3.5/8 AIRFOIL

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HQ 3.5/8 AIRFOILQuabeck HQ 3.5/8 R/C sailplane airfoil
Max thickness 8% at 35% chord
Max camber 3.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hq359-il) HQ 3.5/9 AIRFOIL

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HQ 3.5/9 AIRFOILQuabeck HQ 3.5/9 R/C sailplane airfoil
Max thickness 9% at 35% chord
Max camber 3.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(hs1404-il) HAM-STD HS1-404 AIRFOIL

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HAM-STD HS1-404 AIRFOILHS1 family of prop airfoils from US Patent No. 4
Max thickness 4% at 18% chord
Max camber 3.1% at 46% chord
Source UIUC Airfoil Coordinates Database

(hs1430-il) HAM-STD HS1-430 AIRFOIL

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HAM-STD HS1-430 AIRFOILHS1 family of prop airfoils from US Patent No. 4
Max thickness 30% at 34% chord
Max camber 3% at 44% chord
Source UIUC Airfoil Coordinates Database

(hs1606-il) HAM-STD HS1-606 AIRFOIL

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HAM-STD HS1-606 AIRFOILHS1 family of prop airfoils from US Patent No. 4
Max thickness 6% at 18% chord
Max camber 4.4% at 46% chord
Source UIUC Airfoil Coordinates Database

(hs1620-il) HAM-STD HS1-620 AIRFOIL

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HAM-STD HS1-620 AIRFOILHS1 family of prop airfoils from US Patent No. 4
Max thickness 20% at 34% chord
Max camber 4.1% at 44% chord
Source UIUC Airfoil Coordinates Database

(hs1708-il) HAM-STD HS1-708 AIRFOIL

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HAM-STD HS1-708 AIRFOILHS1 family of prop airfoils from US Patent No. 4
Max thickness 7.9% at 22% chord
Max camber 5% at 46% chord
Source UIUC Airfoil Coordinates Database

(hs1712-il) HAM-STD HS1-712 AIRFOIL

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HAM-STD HS1-712 AIRFOILHS1 family of prop airfoils from US Patent No. 4
Max thickness 12% at 36% chord
Max camber 4.9% at 44% chord
Source UIUC Airfoil Coordinates Database

(hsnlf213-il) HSNLF(1)-0213 AIRFOIL

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HSNLF(1)-0213 AIRFOILNASA/Langley HSNLF(1)-0213 high speed natural laminar flow airfoil
Max thickness 13.3% at 42.4% chord
Max camber 1.4% at 32.4% chord
Source UIUC Airfoil Coordinates Database

(ht05-il) HT05

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HT05Drela HT05 airfoil
Max thickness 4.8% at 17.1% chord
Max camber 0% at 63.3% chord
Source UIUC Airfoil Coordinates Database

(ht08-il) HT08

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HT08Drela HT08 airfoil
Max thickness 5% at 20.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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