My airfoils Airfoil plotter Airfoil comparison Reynolds number calc NACA 4 digit generator NACA 5 digit generator Information Airfoil data Lift/drag polars Generated airfoil shapes Searches Symmetrical airfoils NACA 4 digit airfoils NACA 5 digit airfoils NACA 6 series airfoils Airfoils A to Z A a18...
Relativity Group National Center for Supercomputing Applications University of Illinois at Urbana-Champaign Home Page and summary. ONEDBH (no source here?) ONEBH (overview and source) 3D codes front end.NACA airfoils Collection of articles and links related to NACA airfoils is here....
Alphabetic list of airfoils (aerofoils) (U). UA(2)-180 (University Of Alberta/Marsden) to USA 34 AIRFOIL
My airfoils Airfoil plotter Airfoil comparison Reynolds number calc NACA 4 digit generator NACA 5 digit generator Information Airfoil data Lift/drag polars Generated airfoil shapes Searches Symmetrical airfoils NACA 4 digit airfoils NACA 5 digit airfoils NACA 6 series airfoils Airfoils A to Z A a18...
NACA 6 series airfoils Airfoils A to Z A a18 to avistar (88) B b29root to bw3 (22) C c141a to curtisc72 (40) D dae11 to du861372 (28) E e1098 to esa40 (209) F falcon to fxs21158 (121) G geminism to gu255118 (419) H hh02 to ht23 (63) I isa571 to isa962 (...
NACA 6 series airfoils Airfoils A to Z A a18 to avistar (88) B b29root to bw3 (22) C c141a to curtisc72 (40) D dae11 to du861372 (28) E e1098 to esa40 (209) F falcon to fxs21158 (121) G geminism to gu255118 (419) H hh02 to ht23 (63) I isa571 to isa962 (...
You have 0 airfoils loaded.Your Reynold number range is 50,000 to 1,000,000. (set) Applications Airfoil database search My airfoils Airfoil plotter Airfoil comparison Reynolds number calc NACA 4 digit generator NACA 5 digit generator Information Airfoil data Lift/drag polars Generated airfoil ...
Alphabetic list of airfoils (aerofoils) (A). A18 (original) to AG27 Bubble Dancer DLG By Mark Drela
(n0012-il) NACA 0012 AIRFOILS Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file NACA 0012 airfoil Max thickness 12% at 30% chord Max camber 0% at 0% chord SourceUIUC Airfoil Coordinates Database ...
Lockheed-Georgia C-141 transonic wing airfoils Max thickness 12.6% at 40.2% chord Max camber 1.1% at 64.5% chord SourceUIUC Airfoil Coordinates Database (c141c-il) LOCKHEED C-141 BL426.57 AIRFOIL Airfoil details Send to airfoil plotter