2h 2h
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Consider plane inviscid flow through asymmetric diffuser,
as in Fig. C8.3. Only the upper half is shown. The flow is
to expand from inlet half-width h to exit half-width 2h, as
shown. The expansion angle θ is 18.5° (L ≈ 3h). Set up a
nonsquare potential flow mesh for this problem, and calculate and plot (a) the velocity distribution and (b) the
pressure coefficient along the centerline. Assume uniform
inlet and exit flows.
Transcribed Image Text:2h
2h
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