CLARK Y airfoil. The flat bottom simplifies angle measurements on propellers, and makes for easy construction of wings. Je voulais créer une réedition du sempiternel mais toujours efficace Clark Y, qui avec sa facilité de construction (construction à plat) et ses caractéristiques de vol séduit encore beaucoup de modéliste. dat files are parsed and any parser warnings that appear in the form above. Ce dernier est bien meilleur à ce Re que le NM CLassic et que le Clark Y. Les ailerons sont classiquement à mettre à 30% de la corde pour les deux profils, et le profil NM CLassic Saumon en général trouve très bien sa place à partir du dernier quart ou 1/5e de l'aile. hereand they will appear in the list of airfoils in the form below. - Signaler un contenu illicite sur ce site, Quelques news - Profil NM bientot en l'air - Graphen F3F/F3B. [5], An inverted Clark Y airfoil was used on the spoilers of the Dodge Charger Daytona and Plymouth Superbird. Please refer to the information page for details of how the Max thickness 11.7% at 28% chord. The dat file data can either be loaded from the Ce dernier est bien meilleur à ce Re que le NM CLassic et que le Clark Y. Les ailerons sont classiquement à mettre à 30% de la corde pour les deux profils, et le profil NM CLassic Saumon en général trouve très bien sa place à partir du dernier quart ou 1/5e de l'aile. The Clark Y is appealing for its near-flat lower surface, which aids in the construction of wings on plans mounted on a flat construction board. Open paginated plan in new window for multi page printing, Thickness - The dat file Y coordinate is multiplied by the thickness / 100, Reverse - If the reverse tick box is set the Y coordinate is reversed (Y = -Y) to invert the image about the X axis, Origin - The X coordinate is adjusted to move the position of the origin (X = X - (origin / 100) ), Chord width - The X and Y coordinates are multiplied by the chord width to convert the values to millimetres, Radius - If the radius is non zero the X and Y coordinates are transformed around a circle with a centre at X=0 and Y=(radius value). Parser. Max camber 3.4% at … La force de portance augmente avec l’angle d’incidence lorsque celui-ci reste faible, ainsi qu’avec la vitesse. profil NM, MVR et NMR pour le planeur R/C. CIRAS Orléans-Tours B.I.A. [4] The Clark Y was chosen as its flat bottom worked well with the design goal of a low radar cross-section. The Clark YH airfoil is similar but with a reflexed (turned up) trailing edge producing a more positive pitching moment reducing the horizontal tail load required to trim an aircraft. Plot and print the shape of an airfoil (aerofoil) for your specific chord width and transformation. For many applications the Clark Y has been an adequate airfoil section; it gives reasonable overall performance in respect of its lift-to-drag ratio, and has gentle and relatively benign stall characteristics. Créer un site gratuit avec e-monsite The Clark Y has found favor for the construction of model aircraft, thanks to the flight performance that the section offers at medium Reynolds number airflows. Dat file. https://en.wikipedia.org/w/index.php?title=Clark_Y_airfoil&oldid=970319474, Creative Commons Attribution-ShareAlike License, This page was last edited on 30 July 2020, at 16:19. The airfoil has a thickness of 11.7 percent and is flat on the lower surface aft of 30 percent of chord. (clarky-il) CLARK Y AIRFOIL. The flat bottom simplifies angle measurements on propellers, and makes for easy construction of wings. Pitch - The X and Y coordinates are rotated about the origin by the pitch angle. Pour les faibles Reynolds le Clark Y est un peu moins sympa, d'où la création du NM Classic et de son adaptation pour les saumons. The profile was designed in 1922 by Virginius E. Clark. CLARK Y AIRFOIL - CLARK Y airfoil. [1][2], The Lockheed Vega and Spirit of St. Louis are two of the better known aircraft using the Clark Y profile, while the Ilyushin Il-2 and Hawker Hurricane are examples of mass-produced users of the Clark YH.[3]. Some of the better-known aircraft that use the Clark Y and YH: Piccirillo, Albert, "The Clark Y Airfoil - A Historical Retrospective," SAE/AIAA paper 2000-01-5517, presented at the World Aviation Congress & Exposition, October 10, 2000, San Diego, California. Chord width - The X and Y coordinates are multiplied by the chord width to convert the values to millimetres; Radius - If the radius is non zero the X and Y coordinates are transformed around a circle with a centre at X=0 and Y=(radius value) Pitch - The X and Y … airfoil databaseor your own airfoils which can be entered Esthétiquement le NM Classic à 12% ressemble à ça: Lors d'une comparaison directe avec le Clark Y on observe ces polaires: On peut déduire de ce graphique que le NM Classic pour les Cz > 0.4 est assez similaire au clark Y, par contre en deça (0