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MMLU-Pro / 11990 / A supersonic wind-tunnel consists of a large reservoir containing gas under high…

Problem

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question

A supersonic wind-tunnel consists of a large reservoir containing gas under high pressure which is discharged through a convergent-divergent nozzle to a test section of constant cross-sectional area. The cross-sectional area of the throat of the nozzle is 500 mm^2 and the Mach number in the test section is 4. Calculate the cross-sectional area of the test section assuming \gamma = 1.4.

category

engineering

options

  1. 4000 mm^2
  2. 4900 mm^2
  3. 7500 mm^2
  4. 5000 mm^2
  5. 3500 mm^2
  6. 4500 mm^2
  7. 5360 mm^2
  8. 6000 mm^2
  9. 6800 mm^2
  10. 6200 mm^2

src

stemez-FluidMechanics

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