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Airfoil database list (B).

B-29 ROOT AIRFOIL to BOEING 106 AIRFOIL

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(b29root-il) B-29 ROOT AIRFOIL

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B-29 ROOT AIRFOILBoeing B-29 root airfoil
Max thickness 22% at 30.2% chord
Max camber 1.7% at 30.2% chord
Source UIUC Airfoil Coordinates Database

(b29tip-il) B-29 TIP AIRFOIL

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B-29 TIP AIRFOILBoeing B-29 tip airfoil
Max thickness 9% at 30% chord
Max camber 2.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(b540ols-il) BELL 540 AIRFOIL (MODIFIED NACA 0012)

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BELL 540 AIRFOIL (MODIFIED NACA 0012)Bell AH-1 rotor blade airfoil (operational loads survey)
Max thickness 9.7% at 22.1% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(b707a-il) BOEING 707 .08 SPAN AIRFOIL

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BOEING 707 .08 SPAN AIRFOILBoeing Commercial Airplane Company model 707 airfoils
Max thickness 11.4% at 24% chord
Max camber 0.2% at 6% chord
Source UIUC Airfoil Coordinates Database

(b707b-il) BOEING 707 .19 SPAN AIRFOIL

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BOEING 707 .19 SPAN AIRFOILBoeing Commercial Airplane Company model 707 airfoils
Max thickness 12.1% at 29.9% chord
Max camber 0.7% at 9.9% chord
Source UIUC Airfoil Coordinates Database

(b707c-il) BOEING 707 .40 SPAN AIRFOIL

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BOEING 707 .40 SPAN AIRFOILBoeing Commercial Airplane Company model 707 airfoils
Max thickness 9.6% at 30% chord
Max camber 1.9% at 15% chord
Source UIUC Airfoil Coordinates Database

(b707d-il) BOEING 707 .54 SPAN AIRFOIL

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BOEING 707 .54 SPAN AIRFOILBoeing Commercial Airplane Company model 707 airfoils
Max thickness 9% at 40% chord
Max camber 1.8% at 30% chord
Source UIUC Airfoil Coordinates Database

(b707e-il) BOEING 707 .99 SPAN AIRFOIL

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BOEING 707 .99 SPAN AIRFOILBoeing Commercial Airplane Company model 707 airfoils
Max thickness 9% at 42% chord
Max camber 1.8% at 34% chord
Source UIUC Airfoil Coordinates Database

(b737a-il) BOEING 737 ROOT AIRFOIL

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BOEING 737 ROOT AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 15.4% at 19.6% chord
Max camber 0.2% at 5% chord
Source UIUC Airfoil Coordinates Database

(b737b-il) BOEING 737 MIDSPAN AIRFOIL

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BOEING 737 MIDSPAN AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 12.5% at 29.7% chord
Max camber 0.8% at 10% chord
Source UIUC Airfoil Coordinates Database

(b737c-il) BOEING 737 MIDSPAN AIRFOIL

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BOEING 737 MIDSPAN AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 10% at 39.9% chord
Max camber 1.5% at 20.4% chord
Source UIUC Airfoil Coordinates Database

(b737d-il) BOEING 737 OUTBOARD AIRFOIL

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BOEING 737 OUTBOARD AIRFOILBoeing Commercial Airplane Company model 737 airfoils
Max thickness 10.8% at 40% chord
Max camber 1.6% at 20% chord
Source UIUC Airfoil Coordinates Database

(bacj-il) BOEING AIRFOIL J (no closed TE)

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BOEING AIRFOIL J (no closed TE)Boeing Commercial Airplane Company airfoil J
Max thickness 10.1% at 40% chord
Max camber 1.7% at 78% chord
Source UIUC Airfoil Coordinates Database

(bacnlf-il) BOEING HSNLF AIRFOIL

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BOEING HSNLF AIRFOILBoeing high speed natural laminar flow airfoil from a European patent (EP 0111785A1)
Max thickness 10.1% at 43.7% chord
Max camber 1.3% at 76.7% chord
Source UIUC Airfoil Coordinates Database

(bacxxx-il) BOEING BACXXX AIRFOIL

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BOEING BACXXX AIRFOILBoeing Commercial Airplane Company BACXXX Energy Efficient Transport Program airfoil
Max thickness 11.3% at 35% chord
Max camber 1.4% at 15% chord
Source UIUC Airfoil Coordinates Database

(bambino6-il) Bambino 6

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Bambino 6Bambino 6 airfoil
Max thickness 12% at 40% chord
Max camber 2.8% at 40% chord
Source UIUC Airfoil Coordinates Database

(be50-il) BE50 (original)

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BE50 (original)Verbitsky BE50 free flight airfoil (original)
Max thickness 7.3% at 25% chord
Max camber 4.1% at 45% chord
Source UIUC Airfoil Coordinates Database

(be50sm-il) BE50 (smoothed)

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BE50 (smoothed)Verbitsky BE50 free flight airfoil (original)
Max thickness 7.3% at 23.8% chord
Max camber 4% at 45.4% chord
Source UIUC Airfoil Coordinates Database

(boe103-il) BOEING 103 AIRFOIL

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BOEING 103 AIRFOILBoeing 103 airfoil
Max thickness 12.7% at 30% chord
Max camber 3.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(boe106-il) BOEING 106 AIRFOIL

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BOEING 106 AIRFOILBoeing 106 airfoil
Max thickness 13.1% at 30% chord
Max camber 3.3% at 40% chord
Source UIUC Airfoil Coordinates Database
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