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aircraft:tmd:aerofuselage [2017/01/23 18:43] – jhaircraft:tmd:aerofuselage [2018/09/30 13:33] – [Minimal] jh
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 === Other aerodynamic classes === === Other aerodynamic classes ===
-[[aerowing]], [[airfoil]], [[airbrake]], [[propeller]], [[aerodrag]], [[bladeforce]], [[bodyaerodynamics]]+[[aerowing]], [[airfoil]], [[airbrake]], [[propeller]], [[aerodrag]], [[bladeforce]]
  
 ===== Stations ===== ===== Stations =====
Line 96: Line 96:
  
 > The ''Cm'' of the fuselage is not the ideal parameter to make an aircraft more agile around the pitch axis. Use [[aerowing#downwash|aerowing downwash]] and the [[airfoil#cmalpha|airfoil CmAlpha]] parameters. > The ''Cm'' of the fuselage is not the ideal parameter to make an aircraft more agile around the pitch axis. Use [[aerowing#downwash|aerowing downwash]] and the [[airfoil#cmalpha|airfoil CmAlpha]] parameters.
 +
 +=== Propeller ===
 +
 +The ''LateralForceCoefficient'' and ''LateralDragCoefficient'' of a [[propeller]] also have a large influence on the knife edge flight. (Please see main topic about the [[propeller]] class)
  
 ===== Example Code ===== ===== Example Code =====
  
 ==== Minimal ==== ==== Minimal ====
-<code>       <[string8][object][aerofuselage] + 
-            <[string8][Name][FuselageAero]> +> **Caution**: Requires a [[rigidbody]] with the name ''Fuselage'' 
-            <[string8][Body][Fuselage]> + 
-            <[float64tmarray][StationX]     [ 0.000000 -1.000000 ]> +<code>           <[aerofuselage][FuselageAero][] 
-            <[float64tmarray][StationY]     [ 0.000000  0.000000 ]> +                <[string8][Body][Fuselage]> 
-            <[float64tmarray][StationZ]     [ 0.000000  0.000000 ]> +                <[float64tmarray][StationX]     [ 1.0 -1.0  ]> 
-            <[float64tmarray][StationWidth] [ 0.000000  0.200000 ]> +                <[float64tmarray][StationY]     [ 0.0  0.0  ]> 
-            <[float64tmarray][StationHeight][ 0.000000  0.250000 ]> +                <[float64tmarray][StationZ]     [ 0.0  0.0  ]> 
-            <[uint32tmarray][StationShape]  [ 1         1        ]> +                <[float64tmarray][StationWidth] [ 0.05 0.05 ]> 
-            <[float64][Cdx][0.05]> +                <[float64tmarray][StationHeight][ 0.05 0.05 ]> 
-            <[float64][Cdy][1.00]> +                <[uint32tmarray][StationShape]  [ 0    0    ]> 
-            <[float64][Cdz][1.00]> +                <[float64][Cdx][0.05]> 
-            <[float64][Cly][1.00]> +                <[float64][Cdy][0.8]> 
-            <[float64][Clz][1.00]> +                <[float64][Cdz][0.8]> 
-        ></code>+                <[float64][Cly][0.6]> 
 +                <[float64][Clz][0.6]> 
 +                <[float64][Cm] [0.0]> 
 +            ></code>
                  
 ==== All ==== ==== All ====
-<code>       <[string8][object][aerofuselage] + 
-            <[string8][Name][FuselageAero]> +> **Caution**: Requires a [[rigidbody]] with the name ''Fuselage'' 
-            <[string8][Body][Fuselage]> + 
-            <[tmvector3d][R0][0.000000 0.000000 0.000000]> +<code>           <[aerofuselage][FuselageAero][] 
-            <[tmvector3d][X0][1.000000 0.000000 0.000000]> +                <[string8][Body][Fuselage]> 
-            <[tmvector3d][Y0][0.000000 1.000000 0.000000]> +                <[tmvector3d][R0][ 0.0 0.0 0.0 ]> 
-            <[tmvector3d][Z0][0.000000 0.000000 1.000000]> +                <[tmvector3d][X0][ 1.0 0.0 0.0 ]> 
-            <[float64tmarray][StationX]     [ 1.000000  0.500000 -0.500000 -2.000000 ]> +                <[tmvector3d][Y0][ 0.0 1.0 0.0 ]> 
-            <[float64tmarray][StationY]     [ 0.000000  0.000000  0.000000  0.000000 ]> +                <[tmvector3d][Z0][ 0.0 0.0 1.0 ]> 
-            <[float64tmarray][StationZ]     [ 0.000000  0.000000  0.000000  0.000000 ]> +                <[float64tmarray][StationX]     [ 1.0  0.5  -0.5   -2.0  ]> 
-            <[float64tmarray][StationWidth] [ 0.000000  0.200000  0.100000  0.050000 ]> +                <[float64tmarray][StationY]     [ 0.0  0.0   0.0    0.0  ]> 
-            <[float64tmarray][StationHeight][ 0.000000  0.250000  0.125000  0.050000 ]> +                <[float64tmarray][StationZ]     [ 0.0  0.0   0.0    0.0  ]> 
-            <[uint32tmarray][StationShape]  [ 0         1         1         0        ]> +                <[float64tmarray][StationWidth] [ 0.0  0.2   0.1    0.05 ]> 
-            <[float64][Cdx][0.05]> +                <[float64tmarray][StationHeight][ 0.0  0.25  0.125  0.05 ]> 
-            <[float64][Cdy][1.50]> +                <[uint32tmarray][StationShape]  [ 0    1     1      0    ]> 
-            <[float64][Cdz][1.50]> +                <[float64][Cdx][0.05]> 
-            <[float64][Cly][1.50]> +                <[float64][Cdy][0.8]> 
-            <[float64][Clz][1.50]> +                <[float64][Cdz][0.8]> 
-            <[float64][Cm][-0.00]> +                <[float64][Cly][0.6]> 
-            <[float64][Offset][0.000000]> +                <[float64][Clz][0.6]> 
-            <[bool][HasSwimmer][false]> +                <[float64][Cm] [0.0]> 
-        ></code>+                <[float64][Offset][0.0]> 
 +                <[bool][HasSwimmer][false]> 
 +            ></code>
  
aircraft/tmd/aerofuselage.txt · Last modified: 2019/07/07 10:50 by jh