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aircraft:tmd:airfoil [2017/03/06 11:28] – [Table of flap coefficients] jhaircraft:tmd:airfoil [2018/09/30 13:20] – [Minimal] jh
Line 4: Line 4:
  
 === Other Aerodynamic classes === === Other Aerodynamic classes ===
-[[aerowing]], [[aerofuselage]], [[airbrake]], [[propeller]], [[aerodrag]], [[bladeforce]], [[bodyaerodynamics]]+[[aerowing]], [[aerofuselage]], [[airbrake]], [[propeller]], [[aerodrag]], [[bladeforce]]
  
 ===== Angle of attack ===== ===== Angle of attack =====
Line 146: Line 146:
 ==== Minimal ==== ==== Minimal ====
 This will fall back to default values for all attributes. This will fall back to default values for all attributes.
-<code>        <[string8][object][airfoil+<code>            <[airfoil][AirfoilTip][] 
-            <[string8][Name][AirfoilTip]> +            ></code>
-        ></code>+
                  
 ==== All ===== ==== All =====
-<code>        <[string8][object][airfoil] +<code>            <[airfoil][NACA0009][] 
-            <[string8][Name][AirfoilTip]> +                <[float64][Cl0][0.0]> 
-            <[float64][Cl0][0.0]> +                <[float64][Cd0][0.007]> 
-            <[float64][Cd0][0.007]> +                <[float64][Cm0][0.0]> 
-            <[float64][Cm0][0.0]> +                <[float64][ClAlpha][6.28]> 
-            <[float64][ClAlpha][6.28]> +                <[float64][CdAlpha][0.4]> 
-            <[float64][CdAlpha][0.4]> +                <[float64][CmAlpha][0.0]> 
-            <[float64][CmAlpha][0.0]> +                <[float64][ClFlap][2.1]> 
-            <[float64][ClFlap][2.1]> +                <[float64][CdFlap][0.05]> 
-            <[float64][CdFlap][0.0]> +                <[float64][CmFlap][-0.3]> 
-            <[float64][CmFlap][-0.2]> +                <[float64][Cd0Base][0.005]> 
-            <[float64][Cd0Base][0.005]> +                <[float64][ClAlphaBase][2.4]> 
-            <[float64][ClAlphaBase][2.4]> +                <[float64][CdAlphaBase][1.8]> 
-            <[float64][CdAlphaBase][1.8]> +                <[float64][CmAlphaBase][-0.45]> 
-            <[float64][CmAlphaBase][-0.2]> +                <[float64][AttachedCenter][0.0]> 
-            <[float64][ClFlapBase][0.5]> +                <[float64][AttachedRange][0.17]> 
-            <[float64][AttachedCenter][0.0]> +                <[float64][StallRange][0.1]> 
-            <[float64][AttachedRange][0.25]> +                <[float64][ClFlapBase][0.5]> 
-            <[float64][StallRange][0.25]> +                <[float64][AttachedCenterFlap][-0.12]> 
-            <[float64][AttachedCenterFlap][-0.12]> +            ></code>
-        ></code>+
  
aircraft/tmd/airfoil.txt · Last modified: 2020/09/28 22:44 by jh