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- Subject
- Fluid Mechanics for Chemicalchemical-engineering › fluid-mechanics-for-chemical-chemical-engineering
- Published
- 11 Mar 2019
- Last updated
- 28 May 2026
Explanation
Option A is true because the Mach number reaches unity at the throat of the nozzle. Option B is correct since no shock waves occur within the nozzle when the exit Mach number is supersonic. Option C is incorrect because density typically decreases downstream in the converging part due to acceleration. Therefore, the correct choice is option B.
More Fluid Mechanics for Chemical MCQs
Practice related questions from the same subject.
- 1.Identify the incorrect statement from the following:
- 2.Identify the incorrect statement from the following:
- 3.Identify the incorrect statement from the following:
- 4.Which of the following statements about a Venturimeter is accurate?
- 5.Which of the following statements is accurate?
- 6.Identify the incorrect statement regarding a streamline.
- 7.Identify the incorrect statement from the following options:
- 8.Identify the incorrect statement from the following options:
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