Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

Airfoil database list (M).

MH 24 9.01% to MH 80 12.72%

Page 4 of 5     1 2 3 4 5     Next

(mh24-il) MH 24 9.01%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 24  9.01%Martin Hepperle MH 24 for F3D Pylon Racing (extended laminar flow)
Max thickness 9% at 37.3% chord
Max camber 1.2% at 37.3% chord
Source UIUC Airfoil Coordinates Database

(mh25-il) MH 25 9.98%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 25  9.98%Martin Hepperle MH 25 for F3D Pylon Racing (extended laminar flow)
Max thickness 10% at 42.2% chord
Max camber 1.4% at 42.2% chord
Source UIUC Airfoil Coordinates Database

(mh26-il) MH 26 10.99%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 26  10.99%Martin Hepperle MH 26 for F3D Pylon Racing (extended laminar flow)
Max thickness 11% at 42.3% chord
Max camber 1.4% at 42.3% chord
Source UIUC Airfoil Coordinates Database

(mh27-il) MH 27 11.99%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 27  11.99%Martin Hepperle MH 27 for F3D Pylon Racing (extended laminar flow)
Max thickness 12% at 42.4% chord
Max camber 1.4% at 42.4% chord
Source UIUC Airfoil Coordinates Database

(mh30-il) MH 30 7.84%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 30  7.84%Martin Hepperle MH 30 for F3E and F3B
Max thickness 7.8% at 31% chord
Max camber 1.7% at 46.4% chord
Source UIUC Airfoil Coordinates Database

(mh32-il) MH 32 8.7%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 32  8.7%Martin Hepperle MH 32 for F3E and F3B
Max thickness 8.7% at 30.2% chord
Max camber 2.3% at 45.7% chord
Source UIUC Airfoil Coordinates Database

(mh33-il) MH33

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH33Martin Hepperle MH 33 for F3E and F3B
Max thickness 7.3% at 29.3% chord
Max camber 1.1% at 43.9% chord
Source UIUC Airfoil Coordinates Database

(mh38-il) MH 38 9.68%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 38  9.68%Martin Hepperle MH 38 for Endurance Model
Max thickness 9.7% at 31.6% chord
Max camber 3.9% at 45.3% chord
Source UIUC Airfoil Coordinates Database

(mh42-il) MH 42 8.94%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 42  8.94%Martin Hepperle MH 42 low Reynolds number airfoil
Max thickness 8.9% at 31.3% chord
Max camber 1.8% at 36.3% chord
Source UIUC Airfoil Coordinates Database

(mh43-il) MH 43 8.5%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 43  8.5%Martin Hepperle MH 43 for F3B and F3E
Max thickness 8.5% at 31.4% chord
Max camber 1.7% at 36.4% chord
Source UIUC Airfoil Coordinates Database

(mh44-il) MH 44 9.66%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 44  9.66%Martin Hepperle MH 44 for flying wings
Max thickness 9.6% at 27.1% chord
Max camber 1.5% at 36.9% chord
Source UIUC Airfoil Coordinates Database

(mh45-il) MH 45 9.85%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 45  9.85%Martin Hepperle MH 45 for flying wings
Max thickness 9.8% at 26.9% chord
Max camber 1.7% at 36.6% chord
Source UIUC Airfoil Coordinates Database

(mh46-il) MH 46 9.1%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 46  9.1%Martin Hepperle MH 46 for flying wings
Max thickness 9.1% at 27.1% chord
Max camber 1.4% at 36.9% chord
Source UIUC Airfoil Coordinates Database

(mh60-il) MH 60 10.08%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 60  10.08%Martin Hepperle MH 60 for flying wings
Max thickness 10.1% at 26.9% chord
Max camber 1.7% at 36.6% chord
Source UIUC Airfoil Coordinates Database

(mh61-il) MH 61 10.26%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 61  10.26%Martin Hepperle MH 61 for flying wings
Max thickness 10.2% at 27.6% chord
Max camber 1.4% at 37.3% chord
Source UIUC Airfoil Coordinates Database

(mh62-il) MH 62 9.3%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 62  9.3%Martin Hepperle MH 62 for flying wings
Max thickness 9.3% at 26.9% chord
Max camber 1.6% at 36.6% chord
Source UIUC Airfoil Coordinates Database

(mh64-il) MH 64 8.59%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 64  8.59%Martin Hepperle MH 64 for flying wings
Max thickness 8.6% at 26.9% chord
Max camber 1.4% at 41.8% chord
Source UIUC Airfoil Coordinates Database

(mh70-il) MH 70 11.08%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 70  11.08%Martin Hepperle MH 70 for fying wing (full size)
Max thickness 11.1% at 29.4% chord
Max camber 3% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(mh78-il) MH 78 14.47%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 78  14.47%Martin Hepperle MH 78 for flying wings (hang glider)
Max thickness 14.4% at 22.1% chord
Max camber 1.9% at 17.9% chord
Source UIUC Airfoil Coordinates Database

(mh80-il) MH 80 12.72%

Airfoil details
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file
Source dat file
MH 80  12.72%Martin Hepperle MH 80 for flying wings (hang glider)
Max thickness 12.7% at 21.7% chord
Max camber 2.8% at 21.7% chord
Source UIUC Airfoil Coordinates Database
Page 4 of 5     1 2 3 4 5     Next

Please see the source web site or designer for any license conditions.