Aerodynamics Practice Test: Numerical Techniques for Steady Supersonic Flow — Flashcards | Aircraft & Aviation | FatSkills

Aerodynamics Practice Test: Numerical Techniques for Steady Supersonic Flow — Flashcards

Fast review mode: answers are shown by default so you can skim quickly. Hide them if you want to self-test.

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.
 

1 of 15 Ready
What is the value of derivative of flow field along characteristic line?
Indeterminate
Shortcuts
Prev Space Show / hide Next
Turn this into a study set.
Sign in with Google to save tricky questions to your reminder list and resume on any device.
Sign in with Google Free • no extra password