(tempest1-il) HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | Hawker Tempest 37.5% semispan airfoil (NPL?) Max thickness 14.5% at 38.3% chord Max camber 1% at 40.4% chord Source UIUC Airfoil Coordinates Database
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(tempest2-il) HAWKER TEMPEST 61% SEMISPAN AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | Hawker Tempest 61% semispan airfoil (NPL?) Max thickness 12% at 37.3% chord Max camber 0.9% at 39.3% chord Source UIUC Airfoil Coordinates Database
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(tempest3-il) HAWKER TEMPEST 96.77% SEMISPAN AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | Hawker Tempest 96.77% semispan airfoil (NPL?) Max thickness 10% at 38.7% chord Max camber 1% at 40.7% chord Source UIUC Airfoil Coordinates Database
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(th25816-il) TH 25816 HALE AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | Naval Air Development Center/Doug Hall high altitude Max thickness 25.7% at 48.3% chord Max camber 4% at 52.9% chord Source UIUC Airfoil Coordinates Database
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(trainer60-il) TRAINER60 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | Great Planes R/C Trainer 60 airfoil Max thickness 18.3% at 27.1% chord Max camber 0.1% at 1.3% chord Source UIUC Airfoil Coordinates Database
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(tsagi-r-3a-il) TsAGI R-3a (12%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | TsAGI R-3a used on Russian ultra light aircraft (12%). Max thickness 12.1% at 23.1% chord Max camber 3.1% at 24.1% chord Source UIUC Airfoil Coordinates Database
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(tsagi12-il) TSAGI 12% AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | TSAGI 12% airfoil Max thickness 11.9% at 30% chord Max camber 2% at 30% chord Source UIUC Airfoil Coordinates Database
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(tsagi8-il) TSAGI 8% AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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 | TSAGI 8% airfoil Max thickness 8% at 30% chord Max camber 1.3% at 30% chord Source UIUC Airfoil Coordinates Database
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