NewtonianAeroPropertiesFromOBJFile:

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   Computes the normal coefficient of a body in hypersonic flow.
   Since version 1.0
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   Form:
   Initialization:
   [cN, normalVec, area, g] = NewtonianAeroPropertiesFromOBJFile( vInf, fileName )
   Aero Property Calculation:
   [cN, normalVec, area, g] = NewtonianAeroPropertiesFromOBJFile( vInf, g )
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   Inputs
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   vInf             (3,1) Free stream velocity vector in body frame (any units)
   fileName         (1,:) File name or data structure

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   Outputs
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   cN               (1,1) Normal coefficient  
   normalVec        (3,1) Unit vector in the direction of the normal
   area             (1,1) Total surface area
   g                 (.)  Data structure with geometry information

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Children:

AeroUtils: CAD/LoadCAD
Common: Graphics/PolygonProps
Math: Linear/Mag
Math: Linear/Unit