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Which of these flows can be modelled by the panel method?(a) Compressible flow(b) Rotational flow(c) Incompressible flow(d) Supersonic flowI had been asked this question in an online quiz.My question is from General Three Dimensional Flows-Panel Techniques topic in portion Three-Dimensional Incompressible Flow of Aerodynamics

Answer»

Correct choice is (c) Incompressible flow

To elaborate: Panel method is IDEA for design ANALYSIS for only incompressible flows. It lacks the ability to model viscous flow, rotational flow w and supersonic flow. A panel method performs best when MODELING fully-attached, high-reynolds-number (> 105), subsonic (Mach number < 1) flow.



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