NACA 5 digit Airfoil Generator
"naca5gen.m" Generates the NACA 5 digit airfoil coordinates with desired no. of panels (line elements) on it.
FEATURES:
*Accurate coordinate generation with the required precision
*Option to generate closed or open Trailing Edge
*Additional separate outputs for camber line, upper surface and lower surface
*A tst (test) file included
INPUTS:
[1] NACA 5 digit designation (eg. '23012')
[2] No of panels (line elements) PER SIDE (upper/lower)
[3] Type of chord station spacing (Half cosine spacing / Uniform spacing)
OUTPUTS:
[1] One can plot the generated airfoil, camber line and the leading edge circle by setting an option input wantPlot=1
[2] A data file can be generated by setting the option input wantFile=1
EXTENSION:
Being a function, the airfoil generator can be called several times from a loop to generate any number of airfoil data files.
引用格式
J. Divahar (2024). NACA 5 digit Airfoil Generator (https://www.mathworks.com/matlabcentral/fileexchange/23241-naca-5-digit-airfoil-generator), MATLAB Central File Exchange. 检索来源 .
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- Aerospace > Aerospace Blockset > Guidance, Navigation, and Control (GNC) >
- Industries > Aerospace and Defense > Airfoil tools >
- Aerospace > Aerospace Toolbox > Standard Workflow Procedures > Coordinate Systems >
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1.0.0.0 |