(k1-il) NYU/GRUMMAN K-1 AIRFOIL | Airfoil details
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 | NYU/Grumman K-1 transonic airfoil (GAC .75-.63-11.6)
Max thickness 11.6% at 33% chord
Max camber 1.9% at 75% chord
Source UIUC Airfoil Coordinates Database
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(k2-il) GRUMMAN K-2 AIRFOIL | Airfoil details
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 | Grumman K-2 transonic airfoil (GAC .80-.53-10.3)
Max thickness 10.3% at 38.9% chord
Max camber 1.3% at 88.3% chord
Source UIUC Airfoil Coordinates Database
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(k3-il) GRUMMAN K-3 AIRFOIL | Airfoil details
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 | Grumman K-3 transonic airfoil (GAC .70-.83-17.5)
Max thickness 17.3% at 33.1% chord
Max camber 2.6% at 74.7% chord
Source UIUC Airfoil Coordinates Database
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(k3311-il) K3311 (original) | Airfoil details
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 | Leon Kincaid K3311 airfoil (original)
Max thickness 11% at 30% chord
Max camber 3.3% at 40% chord
Source UIUC Airfoil Coordinates Database
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(k3311sm-il) K3311 (smoothed) | Airfoil details
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 | Leon Kincaid K3311 airfoil (smoothed)
Max thickness 11% at 30.6% chord
Max camber 3.2% at 41.6% chord
Source UIUC Airfoil Coordinates Database
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(kc135a-il) KC-135 BL52.44 AIRFOIL | Airfoil details
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 | Boeing KC-135 transonic airfoils
Max thickness 15.5% at 35% chord
Max camber 1.3% at 20% chord
Source UIUC Airfoil Coordinates Database
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(kc135b-il) KC-135 BL124.32 AIRFOIL | Airfoil details
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 | Boeing KC-135 transonic airfoils
Max thickness 13% at 40% chord
Max camber 1.4% at 20% chord
Source UIUC Airfoil Coordinates Database
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(kc135c-il) KC-135 BL200.76 AIRFOIL | Airfoil details
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 | Boeing KC-135 transonic airfoils
Max thickness 10.6% at 40% chord
Max camber 1.5% at 25% chord
Source UIUC Airfoil Coordinates Database
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(kc135d-il) KC-135 BL351.6 AIRFOIL | Airfoil details
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 | Boeing KC-135 transonic airfoils
Max thickness 9% at 40% chord
Max camber 1.9% at 30% chord
Source UIUC Airfoil Coordinates Database
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(kc135winglet-il) KC-135 Winglet (supercritical Whitcomb) | Airfoil details
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 | Boeing KC-135 winglet airfoil designed by Richard T. Whitcomb
Max thickness 8% at 40% chord
Max camber 2.7% at 65% chord
Source UIUC Airfoil Coordinates Database
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(kenmar-il) KENNEDY AND MARSDEN AIRFOIL | Airfoil details
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 | University of Alberta/Kennedy and Marsden high lift airfoil
Max thickness 27.9% at 31% chord
Max camber 7.7% at 36.9% chord
Source UIUC Airfoil Coordinates Database
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