Xush kelibsiz, bu yerda o'zgartirilgan versiyasi: ```csharp class PaperPlanePhysics { // Physical constants public float rho = 1.2041f; // air pressure in kg/m3 // Parameters of the paper plane public float surfaceWingArea; // Wing surface area in m2 public float liftCoefficient; // Lift coefficient public float airResistanceCoefficient; // Air resistance coefficient // Compute the lift public float ComputeLiftfloat v) { return 0.5f * rho * v* v* surfaceWingArea * liftCoefficient; } // Compute the drag public float ComputeDrag float v) { return 0.5f * rho * v* v* surfaceWingArea * airResistanceCoefficient } // Calculate the resulting wind resistance
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