If the flow conditions at point 1 near the nozzle wall is given, then what is the flow conditions at point 2 on the wall?

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Aerodynamics Practice Test: Numerical Techniques for Steady Supersonic Flow — practice the complete quiz, review flashcards, or try a random question.

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.
 


If the flow conditions at point 1 near the nozzle wall is given, then what is the flow conditions at point 2 on the wall?<br /><img src='https://www.fatskills.com/engineering/aerodynamics-questions-answers-determination-compatibility-equations-q7.png' alt='Find the flow conditions for the given wall at point 2 if point 1 is given' width='346' height='297' class='alignnone size-full wp-image-326321' />