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Your Reynold number range is 50,000 to 1,000,000. (set)

Airfoil database list (H).

HT12 to HT23

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(ht12-il) HT12

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HT12Drela HT12 airfoil
Max thickness 5% at 18.6% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ht22-il) HT22

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HT22Drela HT22 airfoil
Max thickness 5.1% at 19.1% chord
Max camber 1.1% at 22.7% chord
Source UIUC Airfoil Coordinates Database

(ht23-il) HT23

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HT23Drela HT23 airfoil
Max thickness 6.5% at 20.8% chord
Max camber 1.1% at 22.6% chord
Source UIUC Airfoil Coordinates Database
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