K+ and K– constant along the characteristic lines related velocity to J+ and J– constants.

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Numerical Techniques for Steady Supersonic Flow topics include: Characteristics philosophy, two dimensional irrotational flow, compatibility equations determination, dependencies domain, steady supersonic flow nozzle design, finite differences basics, macCormack’s technique, boundary conditions, cfl criterion, conservation versus nonconservation form equations.
 


K<sub>+</sub> and K<sub>–</sub> constant along the characteristic lines related velocity to J<sub>+</sub> and J<sub>–</sub> constants.