Name | Modified | Size | Downloads / Week |
---|---|---|---|
NacaFoil_pkg.exe | 2013-08-21 | 182.9 MB | |
NacaFoilv1.1.rar | 2013-08-21 | 210.5 kB | |
NacaFoil-ReadME.txt | 2013-04-24 | 1.4 kB | |
Totals: 3 Items | 183.1 MB | 1 |
NacaFoil v1.1- © vineethcs [1] About: NacaFoil is a stand alone GUI code that can be used to generate 4 digit and 5 digit NACA foils accurately. The co-ordinates can be taken out in form of text, dat or AutoCad scripts. [2]Program Details: [2.1] Entering NACA Number: Enter a valid 4 or 5* digit Naca number. The program will display dynamically the options avialable depending on the entered airfoil. *-Enter 5 digit numbers without reflex and choose the reflex option if needed. [2.2] Entering chord: Enter chord in any units. The data points will be generated in the same unit. [2.3] Entering panels: Enter number of panels as need be. The number of data points generated will be one more than the number of panels. [2.4] Choosing Reflex: Reflex is only enabled for 5 digit airfoils. [2.5] Trailing Edge: Chose open trailing edge if u need a blunt trailing edge else choose closed trailing edge for a sharp trailing edge. [2.6] Data Point Distrubution along Chord: Chose cosine, for a cosine variation of the data points along the chord. This is the default and the best choise for almost all cases as almost all the features of the airfoil can be captured properly by this distribution of points. Chose linear for equidistant point distribution. [3] Reference: http://airfoiltools.com/airfoil/naca5digit