Camber

"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...


Platforms: Matlab

"naca4gen.m" Generates the NACA 4 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...


Platforms: Matlab

An Airfoil plotting program for model aircraft Tracfoil features include where it can draw shetting thickness, Leading Edge (V-notch square stock), Trailing Edge.Build 12 spars rectangular or rond (location in units ou % from L.E or T.E, at position under airfoil, under sheeting ).Build 12 holes...


Platforms: Windows

This program produces documents with 6 sodoku puzzles on a page. The difficulty of the puzzles is adjustable via the program preferences. There are many Sodoku programs where the user solves puzzles on the computer screen but none that I know of that are designed to print them out in a dense...


Platforms: Mac

This Airfoil Analyzer tool is mainly intended to be useful in analyzing and comparing the airfoils' geometrical features and in quick plotting of airfoils . Airfoil Analyzer will be useful in the following the ways,d-OCoDo Upto 3 airfoils can be ploted together in the plot area to compare the...


Platforms: Matlab

This model is a quarter-car five link suspension. The model may be used to understand suspension kinematics (toe, caster, camber, later and longitudinal recession), as well as suspension dynamics (understand load paths when driving over bumpy roads). The model was built in SimMechanicsd-OC?D?,...


Platforms: Matlab

AeroLS is an aerodynamic lifting surface analysis program. This means that it computes the effects of air flowing around thin (planform and camber only, no thickness) wings which are operating at a small angle of attack and sideslip in flow that is subsonic, steady, inviscid, and irrotational....


Platforms: Mac