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Verified Commit ab5bc9f7 authored by Thomas Lambert's avatar Thomas Lambert :helicopter:
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doc(Blade): spindir definition

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......@@ -19,15 +19,16 @@ classdef Blade < handle
% -----
%
% Blade properties:
% nElem - Number of elements, [-]
% dy - Element span, [m]
% y - Element absolute radial position, [m]
% r - Element relative radial position (relative to the total radius), [-]
% area - Element area, [m^2]
% chord - Element chord, [m]
% twist - Element twist (also called stagger angle), [rad]
% iAf - Index of airfoil to use for each element, [-]
% sol - Element solidity, [-]
% nElem - Number of elements, [-]
% dy - Element span, [m]
% y - Element absolute radial position, [m]
% r - Element relative radial position (relative to the total radius), [-]
% area - Element area, [m^2]
% chord - Element chord, [m]
% twist - Element twist (also called stagger angle), [rad]
% iAf - Index of airfoil to use for each element, [-]
% sol - Element solidity, [-]
% spinDir - Rotor spin direction (used for coaxial rotors; 1 = cw, -1 = ccw), [-]
%
% Blade methods:
%
......@@ -44,7 +45,7 @@ classdef Blade < handle
% twist : Twist of the guide stations, [deg] (same size as rad)
% iAf : Index of the airfoil for the guide stations, [-] (same size as rad)
% nElem : Number of elements to mesh the whole blade, [-]
% spinDir : Rotational direction of the current rotor, [-]
% spinDir : Rotor spin direction (used for coaxial rotors; 1 = cw, -1 = ccw), [-]
%
% See also: Rotor, rotare, template, af_tools.Airfoil.
%
......@@ -70,7 +71,7 @@ classdef Blade < handle
chord (1, :) double {mustBePositive} % Element chord, [m]
twist (1, :) double {mustBeFinite} % Element twist (also called stagger angle), [rad]
iAf (1, :) double {mustBePositive} % Index of airfoil to use for each element, [-]
spinDir (1, 1) % Rotational direction of the current rotor, [-]
spinDir (1, 1) = 1 % Rotor spin direction (used for coaxial rotors; 1 = cw, -1 = ccw), [-]
end
properties (SetAccess = private, Dependent)
......
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